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Top 50 Emerging Research Topics in Aerospace Engineering

Research topics Aerospace Engineering

Aerospace engineering is a dynamic field that constantly evolves with technological advancements and the exploration of new frontiers. As we move further into the 21 st century, the aerospace industry faces an array of complex challenges and exciting opportunities. To help guide researchers and enthusiasts, iLovePhD has compiled a list of the Top 50 emerging research topics in the field of aerospace engineering. These topics encompass various aspects of aerospace engineering, including propulsion, materials, aerodynamics, space exploration, and sustainability.

Research Topics in Aerospace Engineering

A. advanced materials and structures.

1. Nanomaterials in Aerospace : Exploring the use of nanomaterials to enhance structural properties and create stronger, lighter, and more durable materials.

2. Bio-Inspired Materials : Research materials inspired by nature, such as biomimetic composites, to improve structural design and performance.

3. Self-Healing Materials : Investigating materials capable of autonomously repairing damage, crucial for increasing the lifespan of aerospace components.

4. 3D Printing in Aerospace : Enhancing the use of additive manufacturing for complex geometries and producing lighter, stronger, and customized components.

5. Smart Materials : Research adaptive materials that change properties in response to external stimuli to improve efficiency and safety in aerospace structures.

B. Advanced Propulsion Systems

6. Electric Propulsion : Studying electric propulsion systems, such as ion drives or electric turbofans, for efficiency and reduced environmental impact.

7. Hybrid Propulsion : Exploring combinations of traditional and alternative fuels for more efficient and environmentally friendly propulsion systems.

8. Micro-propulsion Systems : Researching miniaturized propulsion systems for small satellites and micro-spacecraft.

9. Hypersonic Propulsion : Investigating engines capable of sustained operation at hypersonic speeds for high-speed travel and space applications.

10. Green Propellants : Developing non-toxic, environmentally friendly fuels to reduce the environmental impact of aerospace missions.

C. Autonomous Systems and AI

11 . Autonomous Flight Control : Researching and implementing AI-driven systems for autonomous flight control in unmanned aerial vehicles and aircraft.

12. Decision-Making Algorithms : Developing AI algorithms for autonomous systems to make real-time decisions during complex flight scenarios.

13. Swarm Intelligence in Aerospace : Investigating swarm robotics and AI for coordinated operations of multiple drones or satellites.

14. Predictive Maintenance : Implementing AI to predict and prevent mechanical failures, reducing maintenance costs and enhancing safety.

15. AI in Space Exploration : Utilizing AI for autonomous exploration and decision-making in space missions, such as on Mars or other celestial bodies.

D. Space Debris Management

16. Active Debris Removal: Researching and developing technologies for actively removing space debris to reduce collision risks in orbit.

17. Orbital Traffic Management: Implementing systems to track and manage the growing number of satellites and spacecraft in orbit.

18. Debris Mitigation Strategies : Investigating techniques to design satellites with built-in capabilities to reduce debris creation.

19. Space Situational Awareness: Advancing technologies for better tracking and monitoring space objects to prevent collisions.

20. Deorbiting Technologies: Developing methods to safely deorbit defunct satellites and spacecraft to burn up in the Earth’s atmosphere.

E. Aero-elasticity and Aero-acoustics

21. Aero-elastic Tailoring : Studying how to design aircraft wings to adapt and reduce flutter or oscillations in flight.

22. Noise Reduction Technologies : Research advanced materials and designs to mitigate aircraft noise for improved environmental impact.

23. Structural Health Monitoring : Developing sensors and systems for continuous monitoring of aircraft structures to predict potential failures.

24. Sonic Boom Mitigation : Investigating techniques to reduce the intensity of sonic booms to enable supersonic commercial flights.

25. Aero-acoustic Simulations : Improving computational models to simulate and predict noise generated by aircraft in different conditions.

F. Space Habitats and Life Support Systems

26. Regenerative Life Support Systems : Researching systems that recycle waste and support life sustainably in long-duration space missions.

27. Advanced Thermal Control : Developing efficient thermal management systems for space habitats in extreme conditions.

28. Bioastronautics : Investigating the effects of long-duration space travel on human physiology and mental health.

29. Closed Ecological Systems : Designing self-sufficient systems for life support that mimic Earth’s ecological cycles in space.

30. Space Agriculture : Researching methods to grow food sustainably in space for long-term missions.

G. Aerodynamics and Flow Control

31. Flow Control Technologies : Investigating techniques to control airflow over aircraft surfaces for enhanced efficiency and performance.

32. Drag Reduction Methods : Research ways to minimize drag through innovative design and flow control mechanisms.

33. Supersonic and Hypersonic Aerodynamics : Understanding aerodynamics at high speeds and developing efficient designs for supersonic travel.

34. Unmanned Aerial Vehicles (UAVs) : Advancing aerodynamics specific to drone technology and their varied applications.

35. Biologically Inspired Aerodynamics : Studying aerodynamic principles in nature for innovative aircraft designs.

H. Satellite Communication and Networking

36. 5G and Beyond in Space : Researching the implementation of advanced communication technologies in space for higher data rates and improved connectivity.

37. Inter-Satellite Communication : Studying methods for satellites to communicate with each other, forming constellations for better coverage and data sharing.

38. Secure Satellite Communication : Developing encryption methods and secure communication protocols for satellite networks.

39. Internet of Things (IoT) in Space : Exploring IoT applications for connected devices in space-based systems.

40. Quantum Communication in Space : Investigating the application of quantum technologies for secure and high-speed communication in space.

I. Orbital and Planetary Mechanics

41. Formation Flying and Swarming : Researching the dynamics and control strategies for formations of satellites or spacecraft.

42. Space Traffic Control : Developing methods to regulate the traffic of spacecraft in congested orbits.

43. Planetary Landing and Mobility : Improving landing techniques and mobility systems for planetary exploration missions.

44. Orbital Dynamics of Small Satellites : Studying the unique orbital behaviors and challenges faced by small satellites.

45. Space Weather and its Effects : Understanding the impact of space weather on spacecraft and developing strategies for protection.

J. Aerospace Cybersecurity

46. Avionic Systems Security : Securing critical avionic systems from cyber threats and potential attacks.

47. Satellite Cyber Resilience : Developing resilient and secure systems for satellites against cyber intrusions.

48. Flight Control Systems Security : Ensuring the integrity of flight control systems from cyber threats and vulnerabilities.

49. Secure Communication Networks : Implementing robust Cybersecurity measures in Aerospace communication networks.

50. AI-Powered Cyber Defence : Utilizing AI and machine learning for real-time threat detection and response in aerospace systems.

The aerospace engineering field is continually evolving, with research topics continually adapting to technological advancements , societal needs, and environmental considerations. These emerging areas represent only a fraction of the diverse and dynamic research landscape within aerospace engineering. As technology progresses and new challenges arise, researchers will continue to explore innovative solutions, paving the way for the future of aerospace engineering.

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Department of Aerospace Engineering

• Website http://www.bristol.ac.uk/aerospace/

United Kingdom

Student theses

• 1 - 50 out of 197 results
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3d printing shape-changing double-network hydrogels.

Supervisor: Seddon, A. M. (Supervisor) & Eichhorn, S. (Supervisor)

Student thesis : Doctoral Thesis › Doctor of Philosophy (PhD)

A consideration of geometry in very-low Earth orbit satellites

Supervisor: Berthoud, L. (Supervisor) & Allen, C. B. (Supervisor)

Acoustic Flow Perception in Bats and Applications in Navigation

Supervisor: Windsor, S. P. (Supervisor) & Holderied, M. W. (Supervisor)

Active Thermal Management in FRP Composites via Embedded Vascular Networks

Supervisor: Bond, I. P. (Supervisor) & Lawrie, A. G. W. (Supervisor)

Adaptive Compliant Structures for Fluid Flow Control: A ‘catastrophic’ approach

Supervisor: Pirrera, A. (Supervisor), Groh, R. (Supervisor) & Theunissen, R. (Supervisor)

Adaptive Sampling in Particle Image Velocimetry

Supervisor: Poole, D. (Supervisor) & Allen, C. (Supervisor)

Additive Manufacturing of Soft, Functional Structures for Next-Generation Soft Robotics

Supervisor: Faul, C. F. (Supervisor), Rossiter, J. (Supervisor) & Richards, A. (Supervisor)

A design approach for super-efficient Wrapped Tow Reinforced Hierarchical Space Frames

Supervisor: Woods, B. K. S. (Supervisor), Macquart, T. (Supervisor), Schenk, M. (Supervisor) & Pirrera, A. (Supervisor)

Advanced numerical methods for modelling impact in composite materials

Supervisor: Kawashita , L. F. (Supervisor), Melro, A. R. (Supervisor) & Hallett, S. R. (Supervisor)

Aerial Manipulators for Contact-based Interaction

Supervisor: Richardson, T. S. (Supervisor) & Georgilas , I. (External person) (Supervisor)

Aeroacoustic Characteristics of Static and Dynamic Stall

Supervisor: Azarpeyvand, M. (Supervisor) & Allen, C. (Supervisor)

Aerodynamic noise control using surface treatments

Supervisor: Zang, N. (Supervisor) & Azarpeyvand, M. (Supervisor)

Aeroelastic Tailoring of a Composite Wing with Adaptive Control Surfaces for Optimal Aircraft Performance

Supervisor: Pirrera, A. (Supervisor) & Cooper, J. (Supervisor)

Aeroelastic Tailoring of Composite Aircraft Wings with Uncertainty Quantification for Robust and Reliable Design

A holistic investigation of automated fibre placement’s effect on composite laminate thickness.

Supervisor: Potter, K. (Supervisor)

Student thesis : Doctoral Thesis › Engineering Doctorate (EngD)

Aircraft active inceptor dynamics under vibration loads

Supervisor: Lowenberg, M. (Supervisor), Rezgui, D. (Supervisor), Neild, S. A. (Supervisor) & Rahman, K. (External person) (Supervisor)

Alginate based composite scaffold for biomedical engineering applications

Supervisor: Hamerton, I. (Supervisor), Patil, A. (Supervisor) & Rahatekar, S. (Supervisor)

A Model-Based Framework for Early-Stage Analysis of Spacecraft

Supervisor: Berthoud, L. (Supervisor) & Tryfonas, T. (Supervisor)

A multi-scale reinforced natural composite sandwich panel concept for vibroacoustic applications

Supervisor: Scarpa, F. (Supervisor) & Ivanov, D. (Supervisor)

An adaptive shell model with variable-kinematics for the analysis of laminated structures

Supervisor: Hallett, S. (Supervisor), Kawashita, L. (Supervisor) & Pirrera, A. (Supervisor)

Analysis and Design of Buckling Resistant Thin-Walled Structures via Computationally Efficient 3D Stress Analysis

Supervisor: Pirrera, A. (Supervisor) & Weaver, P. (Supervisor)

Analysis and design of composite panels with Stringer run-outs

Supervisor: Weaver, P. (Supervisor)

Analysis and tailoring of stiffened panels with asymmetries via extended modal nudging

Supervisor: Pirrera, A. (Supervisor), Groh, R. (Supervisor) & Weaver, P. M. (Supervisor)

An Efficient Numerical Framework for Capturing Localised 3D Stress Fields in Laminated Composites

A new aerodynamic model for unsteady separated flow on high aspect ratio flexible wings.

Supervisor: Jones, D. P. (Supervisor) & Gaitonde, A. L. (Supervisor)

An experimental-modelling pitch link formulation for an induced ice damaged blade and its usage in vibration-based rotorcraft-blade health monitoring

Supervisor: Cooper, J. (Supervisor) & Titurus, B. (Supervisor)

Student thesis : Master's Thesis › Master of Science by Research (MScR)

An improved constraint stabilisation technique for Udwadia-Kalaba Formulation

Supervisor: Lowenberg , M. H. (Supervisor) & Neild, S. A. (Supervisor)

An improved description of the bonding and consolidation for overmoulded thermoplastic composite ribbed plates

Supervisor: Hallett, S. R. (Supervisor), Kawashita , L. F. (Supervisor), Gude, M. (External person) (Supervisor) & Kupfer, R. (External person) (Supervisor)

An investigation into the use of a pendulum support rig for aerodynamic modelling

Supervisor: Lowenberg, M. (Supervisor)

A numerical study of a nacre-inspired ballistic armour system

Supervisor: Hallett, S. (Supervisor)

A single camera optical system for the measurement of helicopter blade track and elastic deflection

Supervisor: Lieven, N. (Supervisor)

A spacetime framework for aerodynamics of complex motions

Supervisor: Rendall, T. (Supervisor) & Gaitonde, A. (Supervisor)

A Touchy Subject: Development and Exploration of Tactile Sensing for Perception and Manipulation

Supervisor: Lepora, N. (Supervisor) & Richards, A. (Supervisor)

Automated Dry Fibre Placement and Infusion Process Development for Complex Geometries

Supervisor: Potter, K. (Supervisor), Kim, B. C. (Supervisor) & Giddings, P. (Supervisor)

Automating “design for manufacture” of aerospace composite components

Supervisor: Kratz, J. (Supervisor), Rendall, T. (Supervisor) & Visrolia, A. (External person) (Supervisor)

Autonomous and objective characterisation of composite precursors in manufacturing

Supervisor: Ivanov, D. (Supervisor), Belnoue, J. P. (Supervisor), Hallett, S. R. (Supervisor) & Georgilas, I. (External person) (Supervisor)

Bayesian learning for control in multimodal dynamical systems

Supervisor: Richards, A. (Supervisor) & Ek, C. H. (Supervisor)

Behaviour of pseudo-ductile thin-ply angle-ply laminates under different loading conditions

Supervisor: Wisnom, M. (Supervisor), Bond, I. (Supervisor) & Fuller, J. (Supervisor)

Bifurcation analysis of a semiconductor laser subject to phase conjugate feedback

Supervisor: Krauskopf, B. (Supervisor)

Bioinspired Nonlinear Structures: Elastic Instabilities and Sound Production

Supervisor: Groh, R. (Supervisor), Holderied, M. W. (Supervisor) & Pirrera, A. (Supervisor)

Bio-inspired path planning for unmanned air vehicles in urban environments

Supervisor: Windsor, S. P. (Supervisor) & Richards, A. G. (Supervisor)

Bistable Structures for Morphing Applications Using Anisotropic Shells

Cactus based solids.

Supervisor: Scarpa, F. (Supervisor) & Perriman, A. W. (Supervisor)

Cellulose Composite Fibres for Potential Engineering and Bio-medical Applications

Supervisor: Rahatekar, S. (Supervisor) & Wisnom, M. (Supervisor)

Cellulose Nanocrystal Reinforced Electrospun Composite Nanofibres

Supervisor: Eichhorn, S. (Supervisor) & Trask, R. (Supervisor)

Cellulose nanocrystals-based nanomaterials with aligned microstructures for sustainable energy storage technologies

Supervisor: Eichhorn, S. (Supervisor) & Kim, B. C. (Supervisor)

Characterisation and Selection of Sustainable Discontinuous Natural Fibre Reinforced Polymer Constituents and Their Composites

Supervisor: Eichhorn, S. (Supervisor), Hamerton, I. (Supervisor) & Longana, M. L. (Supervisor)

Characterisation and understanding of viscoelastic leading edge protection solutions used on offshore wind turbines

Supervisor: Ward, C. (Supervisor), Hamerton, I. (Supervisor) & Dyer, K. P. (Supervisor)

Chemo-driven soft pneumatic actuation: from catalysts to neutralisation reactions for oscillating pneumatic systems

Supervisor: Faul, C. F. (Supervisor), Trask, R. (Supervisor) & Dicker, M. (Supervisor)

Composite compliant shell mechanisms: tailoring and characterisation

Supervisor: Ward, C. (Supervisor), O'Donnell, M. (Supervisor) & Schenk, M. (Supervisor)

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Mechanical & Aerospace Engineering Theses & Dissertations

Theses and dissertations published by graduate students in the Department of Mechanical and Aerospace Engineering, College of Engineering, Old Dominion University since Fall 2016 are available in this collection. Backfiles of all dissertations (and some theses) have also been added.

In late Fall 2025, all theses will be digitized and available here. In the meantime, consult the Library Catalog to find older items in print.

Theses/Dissertations from 2024 2024

Thesis: Effect of Lunar Magnetic Field and Lunar Regolith Simulant on the Growth and Bioactive Compounds Production of Chlorella Vulgaris Microalgae , Jeries Philip Butros Abedrabbo

Dissertation: Application of the Fokker-Planck Equation for Quantifying Initial Condition Uncertainty of Reversible Dynamic Systems , Troy S. Newhart

Thesis: Structural Characterization of a TriTruss Module , Lauren M. Simmons

Theses/Dissertations from 2023 2023

Thesis: Switching Methods for Three-Dimensional Rotational Dynamics Using Modified Rodrigues Parameters , Matthew Jarrett Banks

Dissertation: Studies of Flowfields and Dynamic Stability Characteristics of a Quadrotor , Engin Baris

Thesis: Development, Experimental Validation, and Progressive Failure Modeling of an Ultra-Thin High Stiffness Deployable Composite Boom for in-Space Applications , Jimesh D. Bhagatji

Thesis: Design and Implementation of a Launching Method for Free to Oscillate Dynamic Stability Testing , Kristen M. Carey

Thesis: SeaLion CubeSat Mission Architecture Using Model Based Systems Engineering with a Docs as Code Approach , Kevin Yi-Tzu Chiu

Dissertation: RoboRetrieve --In a Dual Role as a Hand-held Surgical Robot and a Collaborative Robot End-effector to Perform Spillage-free Specimen Retrieval in Laparoscopy , Siqin Dong

Thesis: Fabrication of Solid Oxide Fuel Cell Components Using Stereolithography 3D Printing , Hannah Dyer

Thesis: Fusion Bonding Behavior of 3D Printed PA6/CF Composites Via Post Fabrication Compaction , Gonzalo Fernandez Mediavilla

Dissertation: Machine Learning Approach to Activity Categorization in Young Adults Using Biomechanical Metrics , Nathan Q. C. Holland

Thesis: Study of Microphonic Effects on the C100 Cryomodule for High Energy Electron Beam Accelerators , Caleb James Hull

Dissertation: E-Cadherin Force Transmission and Stiffness Sensing , Mazen Mezher

Thesis: Experimental and Computational Aerodynamic Studies of Axially-Oriented Low-Fineness-Ratio Cylinders , Forrest Miller

Thesis: The Effect of Through Thickness Reinforcement Angle on the Disbonding Behavior in Skin-Stringer Configuration , Christopher John Morris

Dissertation: Chemical and Physical Interaction Mechanisms and Multifunctional Properties of Plant Based Graphene in Carbon Fiber Epoxy Composites , Daniel W. Mulqueen

Thesis: Data-Driven Predictive Modeling to Enhance Search Efficiency of Glowworm-Inspired Robotic Swarms in Multiple Emission Source Localization Tasks , Payal Nandi

Dissertation: Fabrication of Smooth SAC305 Thin Films via Magnetron Sputtering and Evaluations of Microstructure, Creep, and Electrical Resistivity , Manish Ojha

Dissertation: Faster, Cheaper, and Better CFD: A Case for Machine Learning to Augment Reynolds-Averaged Navier-Stokes , John Peter Romano II

Thesis: A Comparative Study of Vinti-Based Orbit Propagation and Estimation for CubeSats in Very Low Earth Orbits , Ethan Michael Senecal

Theses/Dissertations from 2022 2022

Thesis: A Comparison of Uniaxial Compressive Response and Inelastic Deformation Mechanisms in Freeze Cast Alumina-Epoxy Composites Without and With Rigid Confinement , Tareq Aljuhari

Thesis: Failure Mode, Effects and Criticality Analysis of a Very Low Earth Orbit CubeSat Mission , Robb Christopher Borowicz

Thesis: A Study of Asymmetric Supersonic Wind Tunnel Nozzle Design , Brittany A. Davis

Thesis: Electromagnetic Modeling of a Wind Tunnel Magnetic Suspension and Balance System , Desiree Driver

Dissertation: Advanced Generalized Predictive Control and Its Application to Tiltrotor Aircraft for Stability Augmentation and Vibration Reduction , Thomas Glen Ivanco

Dissertation: Numerical Simulation of Electroosmotic Flow of Viscoelastic Fluid in Microchannel , Jianyu Ji

Thesis: Assembly of Ceramic Particles in Aqueous Suspensions Induced by High-Frequency AC Electric Field , James E. John IV

Dissertation: The Effect of Soft Tissue and Bone Morphology on the Stresses in the Foot and Ankle , Jinhyuk Kim

Thesis: Development of Modeling and Simulation Platform for Path-Planning and Control of Autonomous Underwater Vehicles in Three-Dimensional Spaces , Sai Krishna Abhiram Kondapalli

Thesis: Deep Learning Object-Based Detection of Manufacturing Defects in X-ray Inspection Imaging , Juan C. Parducci

Dissertation: Utilization of Finite Element Analysis Techniques for Adolescent Idiopathic Scoliosis Surgical Planning , Michael A. Polanco

Thesis: Mechanics of Preimpregnated Fiber Tow Deposition and Compaction , Virginia Meredith Rauch

Dissertation: Role of Structural Hierarchy in Multiscale Material Systems , Siavash Sattar

Thesis: Implementation of an Extended Kalman Filter Using Inertial Sensor Data for UAVs During GPS Denied Applications , Sky Seliquini

Dissertation: Collaborative Robotics Strategies for Handling Non-Repetitive Micro-Drilling Tasks Characterized by Low Structural Mechanical Impedance , Xiangyu Wang

Theses/Dissertations from 2021 2021

Dissertation: Tunable Compressive Mechanical Behavior of Ice-Templated Materials , Sashanka Akurati

Thesis: Analysis of a Non-Equilibrium Vortex Pair as Aircraft Trailing Vortices , Manuel Ayala

Thesis: Modeling Interactions in Concentrated Ceramic Suspensions Under AC Electric Field , Naga Bharath Gundrati

Dissertation: Improved Strain Gage Instrumentation Strategies for Rotorcraft Blade Measurements , Timothy S. Davis

Thesis: A Model-Based Systems Engineering Approach to e-VTOL Aircraft and Airspace Infrastructure Design for Urban Air Mobility , Heidi Selina Glaudel

Dissertation: Development and Applications of Adjoint-Based Aerodynamic and Aeroacoustic Multidisciplinary Optimization for Rotorcraft , Ramiz Omur Icke

Thesis: A New Method for Estimating the Physical Characteristics of Martian Dust Devils , Shelly Cahoon Mann

Thesis: Post-Processing and Characterization of Additive Manufactured Carbon Fiber Reinforced Semi-Crystalline Polymers , Patricia Revolinsky

Thesis: Gradient-Based Tradeoff Design for Engineering Applications , Lena Alexis Royster

Thesis: The Effect of Through Thickness Reinforcement on Debonding Behavior of Skin/Stringer Configuration , Yogaraja Sridhar

Thesis: Empirical Modeling of Tilt-Rotor Aerodynamic Performance , Michael C. Stratton

Thesis: A Digital One Degree of Freedom Model of an Electromagnetic Position Sensor , Michelle Elizabeth Weinmann

Theses/Dissertations from 2020 2020

Thesis: Parametric Study of Residual Stresses in Wire and Arc Additive Manufactured Parts , Hisham Khaled Jamil Abusalma

Thesis: The Effect of Compaction Temperature and Pressure on Mechanical Properties of 3D Printed Short Glass Fiber Composites , Pushpashree Jain Ajith Kumar Jain

Thesis: Numerical Analysis of a Roadway Piezoelectric Harvesting System , Abdul Rahman Badawi

Dissertation: Role of Anisometric Particles in Ice-Templated Porous Ceramic Structure and Mechanical Properties , Mahesh Banda

Thesis: Mechanism of Compaction With Wrinkle Formation During Automatic Stitching of Dry Fabrics and the Size Effect of Compression Molded Discontinuous Fiber-Reinforced Composites , Anibal Benjamin Beltran Laredo

Thesis: Conical Orbital Mechanics: A Rework of Classic Orbit Transfer Mechanics , Cian Anthony Branco

Thesis: Rotorcraft Blade Angle Calibration Methods , Brian David Calvert Jr.

Dissertation: Onboard Autonomous Controllability Assessment for Fixed Wing sUAVs , Brian Edward Duvall

Thesis: A Parametric Analysis of a Turbofan Engine with an Auxiliary Bypass Combustion Chamber – The TurboAux Engine , Kaleab Fetahi

Thesis: Space-Based Countermeasure for Hypersonic Glide Vehicle , Robert Joseph Fowler IV

Thesis: Compaction and Residual Stress Modeling in Composite Manufactured with Automated Fiber Placement , Von Clyde Jamora

Thesis: Trajectory Simulation With Battery Modeling for Electric Powered Unmanned Aerial Vehicles , Ege Konuk

Thesis: Detailed Modeling of the Flash Hydrolysis of Algae for Biofuel-Production in COMSOL Multiphysics , Noah Joseph LeGrand

Thesis: Through-Thickness Reinforcement and Repair of Carbon Fiber Based Honeycomb Structures Under Flexure and Tension of Adhesively Bonded Joints , Aleric Alden Sanders

Thesis: Energy Harvesting Using Flextensional Piezoelectric Energy Harvesters in Resonance and Off-Resonance Modes , Mohamed A. Shabara

Thesis: Thermal Contact Resistance Measurement and Related Uncertainties , Amanda Elizabeth Stark

Thesis: Model Based Systems Engineering for a Venture Class Launch Facility , Walter McGee Taraila

Thesis: A Post-Impact Behavior of Platelet-Based Composites Produced by Compression Molding , Christopher Eugene Ervin Volle

Thesis: Nonlinearity Index Aircraft Spin Motion Analysis With Dynamic Inversion Spin Recovery Controller Design , Jeffry Walker

Thesis: A Study of the Aeroacoustics of Swept Propellers for Small Unmanned Aerial Vehicles , Arthur David Wiedemann

Thesis: Finite Element Analysis Investigation of Hybrid Thin-Ply Composites for Improved Performance of Aerospace Structures , Alana M. Zahn

Theses/Dissertations from 2019 2019

Thesis: Characterization and Optimization of a Propeller Test Stand , Colin Bruce Leighton Benjamin

Dissertation: Endogenous Force Transmission Between Epithelial Cells and a Role for α-Catenin , Sandeep Dumbali

Dissertation: Effect of the Physical Micro-Environment on Cell Adhesion and Force Exertion , Mohamad Eftekharjoo

Thesis: Reducing the Noise Impact of Unmanned Aerial Vehicles by Flight Control System Augmentation , Matthew B. Galles

Thesis: Design and Manufacture of an Inertial Cascade Impactor for Industrial Hygiene Purposes , Hector Joel Gortaire

Thesis: Off Axis Compressive Response of Ice-Templated Ceramics , Rahul Kumar Jujjavarapu

Thesis: Unsupervised-Learning Assisted Artificial Neural Network for Optimization , Varun Kote

Dissertation: Numerical Simulation of Viscoelastic Flow in Micro/Nanochannels , Lanju Mei

Thesis: Comparison of Support Methods for Static Aerodynamic Testing and Validation of a Magnetic Suspension and Balance System , Cameron K. Neill

Thesis: Extension of a Penalty Method for Numerically Solving Constrained Multibody Dynamic Problems , Troy Newhart

Dissertation: Computational Analysis and Design Optimization of Convective PCR Devices , Jung Il Shu

Thesis: Periodic Orbit Analytic Construction In The Circular Restricted Three-Body Problem , Jay Shriram Suryawanshi

Thesis: A CFD Study of Steady Fully Developed Laminar Flow Through a 90-Degree Bend Pipe with a Square Cross-Sectional Area , Subodh Sushant Toraskar

Dissertation: Estimation of Arterial Wall Parameters Via Model-Based Analysis of Noninvasively Measured Arterial Pulse Signals , Dan Wang

Theses/Dissertations from 2018 2018

Thesis: Offshore Wind Energy: Simulating Local Offshore Wind Turbine , Ian P. Aquino

Dissertation: Epithelial Sheet Response to External Stimuli , Yashar Bashirzadeh

Thesis: Anthropomorphically Inspired Design of a Tendon-Driven Robotic Prosthesis for Hand Impairments , Manali Bapurao Bhadugale

Thesis: Aerothermodynamic Analysis of a Mars Sample Return Earth-Entry Vehicle , Daniel A. Boyd

Thesis: Volterra Series Approximation for Multi-Degree of Freedom, Multi-Input, Multi-Output, Aircraft Dynamics , Alexander J. Chen

Dissertation: Simplified, Alternative Formulation of Numerical Simulation of Proton Exchange Membrane Fuel Cell , Russell L. Edwards

Thesis: Distributed Sensing and System Identification of Cantilever Beams and Plates in the Presence of Weak Nonlinearities , Patrick Sean Heaney

Thesis: Dynamic Response Modeling of High Speed Planing Craft with Enforced Acceleration , Brian K. Johnson

Dissertation: Identification and Optimal Linear Tracking Control of ODU Autonomous Surface Vehicle , Nadeem Khan

Dissertation: Design and Implementation of an Artificial Neural Network Controller for Quadrotor Flight in Confined Environment , Ahmed Mekky

Thesis: Gust Alleviation System for General Aviation Aircraft , Lucas Coleman Mills

Thesis: Human-Robot Collaborative Force-Controlled Micro-Drilling for Advanced Manufacturing and Medical Applications , Parimal Mahesh Prajapati

Thesis: Single-Stage, Venturi-Driven Desalination System , Brandon Proetto

Thesis: A Cost Effective Design for a Propeller Thrust/Torque Balance , Nicholas Barrett Sadowski

Dissertation: Understanding the Mechanical Behavior of Costal Cartilage at Their Curved Exterior Surface Via a Tactile Sensor with a Built-In Probe for Distributed-Deflection Detection , Jiayue Shen

Thesis: A Scientific Approach to Understanding the Head Trauma Endured by a Mixed Martial Arts Fighter , John William Michael Sorbello

Thesis: Robocatch: Design and Making of a Hand-Held Spillage-Free Specimen Retrieval Robot for Laparoscopic Surgery , Farid Tavakkolmoghaddam

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As part of the requirements for graduate level degrees, students must complete a thesis for a Master's degree and/or dissertation for a Ph.D. Dissertations and theses are submitted to the academic department and the Graduate College and are made available through the University Library. Since 2010, all theses and dissertations are electronically deposited into IDEALS, the Illinois Digital Environment for Access to Learning and Scholarship, the University's open repository of scholarly content.

ProQuest Dissertations is a comprehensive collection of citations to dissertations and theses worldwide from 1861 to the present day. Full text PDFs are available for many Ph.D. dissertations added since 1997 and some older graduate works.

• IDEALS (UIUC Institutional Repository) Digital copies of theses, data sets, and publications by University of Illinois at Urbana-Champaign faculty and students.
• ProQuest Dissertations and Theses PDF copies of dissertations and theses from U.S. universities.

Aerospace Engineering Dissertations & Theses

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Print Dissertations & Theses

Prior to 2010, print format dissertations and theses were bound and cataloged separately for the Grainger Engineering Library. Prior to 1983, each thesis was shelved by a call number assigned by subject headings. To locate them, search the online catalog for the author’s last name, title word(s) if known, and “theses” and the year granted as subject term(s).

Aerospace Engineering dissertations and theses granted from 1985 to 1999 were assigned Q.629.1T a , followed by the 2-number year, followed by starting letters from the author’s last name. (Example: A 1991 thesis by M. Doyle would be Q.629.1Ta91D). Dissertations and theses granted from 2000 to present were assigned Q.629.1T b , followed by the 2-number year, followed by starting letters from the author’s last name. (Example: A 2006 thesis by H. Dewey would be Q.629.1Tb06De).

Aerospace Engineering - Q. 629.1T

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• China Doctoral Dissertations and Masters’ Theses Full-text Database (CDMD) This link opens in a new window CDMD is a database of dissertations and theses from China, representing nearly 500 PhD-granting institutions and over 775 masters-granting institutions, including the Chinese Academy of Sciences, the Chinese Academy of Social Sciences, and the Chinese Academy of Agriculture, among others. The theses and dissertations are available in Chinese, with an interface in English.
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Index and full text of graduate dissertations and theses from North American and European schools and universities, including the University of California, with full text of most doctoral dissertations from UC Berkeley and elsewhere from 1996 forward. Dissertations published prior to 2009 may not include information about the department from which the degree was granted. 

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Home > Daytona Beach > College of Engineering > PhD Dissertations in Aerospace Engineering

PhD Dissertations in Aerospace Engineering

Dissertations - open access dissertations - open access.

A Computational Analysis of the Aerodynamics and Aeroacoustics of Jets with Fluid Injection , Marco Coderoni

Adaptive Augmentation of Non-Minimum Phase Flexible Aerospace Systems , Michael A. DuPuis

Adaptive Control for a Class of Nonlinear, Time Varying Rotational Systems , John Zelina

Adaptive Control of an Aeroelastic System for Active Flutter Suppression and Disturbance Rejection , Patrick Sterling Downs

Adaptive-Optimal Control of Spacecraft near Asteroids , Madhur Tiwari

A Data Driven Modeling Approach for Store Distributed Load and Trajectory Prediction , Nicholas Peters

Additively Manufactured Dielectric Elastomer Actuators: Development and Performance Enhancement , Stanislav Sikulskyi

Additively Manufactured Flexible Piezoelectric Wave-Based Multifunctional Sensor , Rishikesh Srinivasaraghavan Govindarajan

Aeroacoustics of Supersonic Jet Interacting with Solid Surfaces and its Suppression , Seyyed Saman Salehian

An Online Adaptive Machine Learning Framework for Autonomous Fault Detection , Nolan Coulter

A Numerical and Experimental Evaluation of the Turbulent Heat Flux in a Heated Jet in Crossflow , Michael R. Borghi Jr.

Artificial Intelligence-Assisted Inertial Geomagnetic Passive Navigation , Andrei Cuenca

Autonomous Space Surveillance for Arbitrary Domains , David Zuehlke

A Volume-Force Synthetic Disturbance Approach for High-Fidelity of Unsteady Fluid Structure Interactions , Marina Kazarina

Bi-Modal Excitation of a Supersonic Rectangular Jet , Benjamin Malczewski

Computational Model for Pedestrian Movement and Infectious Diseases Spread During Air Travel: A Molecular Dynamics-Like Numerical Approach , Pierrot Derjany

Contributions to the Understanding of Ship Airwakes Using Advanced Flow Diagnostic Techniques , Dhuree Seth

Contributions to the Understanding of Turbulent Boundary Layers Over Curved Walls , Nicholas Zhu

Damage Control Measures in Composites: Focus on Damage Tolerance of Aerospace Structures , Kais Jribi

Data-Driven Architecture to Increase Resilience In Multi-Agent Coordinated Missions , D. F.

Design, Analysis and Experimental Evaluation of 3D Printed Variable Stiffness Structures , Rossana R. Fernandes

Development of Fault Tolerant Adaptive Control Laws for Aerospace Systems , Andres E. Perez Rocha

Direct Adaptive Control for a Trajectory Tracking UAV , Nirmit Prabhakar

Distributed adaptive control methods for uncertain multiagent systems with coupled dynamics , Islam Aly

Durability and Damage Analysis of Hybrid Multiscale Composites , Suma Ayyagari

Investigation of Bio-Inspired Pin Geometries for Heat Transfer Applications , Anish Prasad

Investigation on the Interaction of an Impinging Jet with Cylinder Wakes , Karthik Krishna

Kinematics of Inter-Ply Interfaces In Composite Manufacturing , Sandeep Chava

Multimode Nonlinear Vibration Analysis of Stiffened Functionally Graded Double Curved Shells in a Thermal Environment , Boutros Azizi

Numerical Treatment of Schrödinger’s Equation for One-Particle and Two-Particle Systems Using Matrix Method , Spatika Dasharati Iyengar

On the Local Heat Transfer Behavior of Supercritical Carbon Dioxide , Neil Sullivan

Optimal Sizing and Control of Hybrid Rocket Vehicles , Srija Ryakam

Piezoresistive Hybrid Nanocomposites for Strain and Damage Sensing: Experimental and Numerical Analysis , Audrey Jean-Miche Gbaguidi

Prediction & Active Control of Multi-Rotor Noise , Samuel O. Afari

Rigid Body Constrained Motion Optimization and Control on Lie Groups and Their Tangent Bundles , Brennan S. McCann

Safety Assurance of Non-Deterministic Flight Controllers in Aircraft Applications , Alfonso Noriega

Scale Interactions within a Perturbed Plane Wall Jet , Shibani Bhatt

Spacecraft Trajectory Planning for Optimal Observability using Angles-Only Navigation , Francisco José Franquiz

State Omniscience for Cooperative Local Catalog Maintenance of Close Proximity Satellite Systems , Chris Hays

Stochastic Model Predictive Control via Fixed Structure Policies , Elias Wilson

Stochastic Point Process Modeling for Engineering Applications , Samarth Motagi

Topology Optimization Using Load Path and Homogenization , Kaveh Gharibi

Trajectory Generation for a Multibody Robotic System: Modern Methods Based on Product of Exponentials , Aryslan Malik

Trustable Adaptive Controllers for Multi-Agent Systems with Actuator Dynamics , Atahan Kurttisi

Unsteady Internal Ballistics of a Hybrid Rocket , Naveen Sri Uddanti

Variable Fidelity Studies in Wake Vortex Evolution, Safety, and Control , Petr Kazarin

Dissertations - ERAU Login Required Dissertations - ERAU Login Required

A Set of Machine Learning Tools for Hazard Relative Navigation, Mapping, and Planetary Landing , Daniel Posada

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Academic Level Undergraduate Masters PhD Others

Aims and Objective

• To design an improved turbofan ramjet engine for sustained hypersonic flights. 
• To analyse the fuel consumption of the engine design and maximum thrust to weight ratio. 
• To analyse impact of varying altitude and weather on the performance of engine.
• To evaluate the design and operational cost of the engine and their service life.
• To analyse the benefits of integration of Artificial intelligence in commercial flights.
• To evaluate the working of AI and its control over the aircraft. 
• To evaluate the provided effective outcomes of the program and its future impact on air travel. 
• The study will also provide the system for autonomous communication for AI based aircraft and their role in flight control.
• To design new and improved aero-dynamic design for commercial aircraft.
• To evaluate the fuel consumption of new design.
• To analyse the integration techniques to upgrade the existing aircraft design to new and improved models.
• To evaluate the cost of maintenance of new design and its performance in unexpected conditions.
• To design a new AI based computer program to guide the satellite in complex system. 
• To analyse the implementation techniques of new design in the existing satellite system.
• To compare the effectiveness of new computer program verses existing programs.
• To analyse the efficiency of the computer program and its maximum handling capacity.
• To design the new and improved design for sustained supersonic flights.
• To determine the maximum sheer, tensile and compressional stress of the material and its behavior in flying conditions. 
• To analyse the cost of material production and its maintenance cost.
• To analyse the service life of the material and the ways to increase it.

The aim of the study is to investigate the simulation of infrared and visual sensors and the computational modelling for developing a new system of hypervelocity terminal guidance of the small asteroids (50-150 in diameter). The research aims to develop the computation software techniques for the signal to noise ratio assessment of IR and visual sensors, assessment of maximum and minimum target detection ranges and the Graphic processing unit (GPU) accelerated simulations of the intercept guidance system on the basis of IR will also be developed. Additionally, the aim of the study is to use the model of scaled polyhedron for objects such as NASA’s OSIRIS Rex Bennu, Rosetta Comet mission 67P/C-G and the 433 Eros asteroid for the development of simulation tools that are GPU-based for the terminal guidance system which is IR based.

Objectives:

The objectives of the study are the following:

• To develop the tracing algorithm of parallelized-ray for the simulation of accurate shadowing of the surface of the comets or asteroid which are of irregular shape.
• To study and consider the approximation of polyhedron solid-angle.
• To investigate the processing of the digital image by using the computational model for the determination of multiple or single effect location to estimate the practical feasibility of modern mission concept of planetary defence of using a multiple interceptor vehicle of kinetic energy or the intercept vehicle of hypervelocity asteroid.

The aim of the study is to conduct a critical analysis of the requirement of modelling for the formulation of value in designing and developing engineering system which is large scale and complex. The research aims to study the satellite networking system of NASA. Therefore, the aim of the study is to assist the designers and developers in transitioning from the old necessities approach to the modelling of value. The research aims to use the design structure matrix which will be attribute-based to elaborate the procedure. Additionally, the research aims at quantifying the loss value because of the required usage. Furthermore, an extended study will be conducted on how the requirement presence has thereby resulted in the designs which are sub-optimal. Through this aim, the importance of using the approach of value over the approach of the requirement will be certainly justified. The overall requirement elimination process is not possible therefore, the study will develop an understanding of each of the requirements as not each requirement possess the same potential impact on the value. This aim will assist in areas like after the designing process completion, where the consumer wants to modify the requirements.

• To assess the requirement impact on the sensitivity and value of these requirements on the finest design.
• To analyze the value gap of to what extent there is a need to capture the uncertainty.
• To study the usage of uncertainty’ probabilistic representation and its importance.

The aim of the study is to develop a model of value for the Unnamed Aircraft Systems (UAS) by taking into consideration the operational, environmental and technical scenarios involved for developing an analysis simulation of the decision in order to rate and analyze various UAS based on its readiness level of technology (TRL) and autonomy level (AL). Furthermore, this will assist in future to analyze the problem between the regulation to analyze the induced inefficiencies and the stakeholder preferences in the operation of UAS because of the requirement of policies. Therefore, the research aims to include utilizing a mixture of different frameworks and tools like decision analysis, Multidisciplinary Design Optimization and the Value-Driven Design to understand and analyze different factors which are involved while operating and designing UAS on a big scale for the use of civil applications and structural health monitoring.

The objective of the study will be:

• To analyze how do the various operational and environmental scenario play a crucial role in the operation of UAS with respect to the task which is being performed.
• To study how the class and physical characters of the UAS associated to the TRL and AL to the performance in the various operational scenario.
• To evaluate whether the model of value-based can be used to conduct an analysis of risk on the UAS operation autonomously on the basis of societal, legal and ethical issues.

The aim of the study is to analyze the new approaches usage in the defence acquisition’ negotiation phase, which will certainly form an important phase. Therefore, the study will analyze the required transition to the value by suggesting a performance-based price and value approach for defence acquisition. Therefore, the study aims to payoff maximization to both the contractor and the government establishing the governmental weapon system. The research will propose bargaining ideas from the game theory and will attempt to offer negotiation for the mathematical foundations.

• To evaluate the effectiveness of game theory for improving the approach of value toward negotiation in performance-based and price based contracting scenario which certainly leads toward improved design system as compare to the one which is achieved through the old methods of driving requirement.
• To determine the player order impact the bargaining game.
• To determine whether a value-based approach joint with negotiation over other aspect be certainly utilized for bridging the gap between the defence acquisition setting contractor and the governmental preferences for the weapon system.

Aim of the study The aim of the study will be “To explore a novel approach methodology for rapid hypersonic flow predictions via surrogate modeling with machine learning and deep learning”. Objectives of the study The objectives of the study will be;

• To explore the processes and modeling approaches involved in machine learning and deep learning.
• To understand the concepts of surrogate-based modeling, optimization, and applications in engineering.
• To review the approaches used for the rapid hypersonic flow predictions via surrogate modeling in the past years.
• To compare the past and current approaches that can be used for the predictions of rapid hypersonic flow.
• To develop a novel methodology for the rapid hypersonic flow predictions and to evaluate machine learning and deep learning.
• To examine the aerodynamic data predictions for transonic flows via a machine learning-based surrogate model.
• To evaluate the surrogate modeling approaches of aerodynamic simulations for multiple operating conditions using machine learning.
• To examine the novel spatial-temporal prediction models for the unsteady wake flows based on a hybrid deep neural network.
• To find out the significance of using the novel approaches for rapid hypersonic flow predictions via surrogate modeling with machine learning and deep learning.

Aim of the study The aim of the study will be “To prepare a systematic review for understanding the effect of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform”. Objectives of the study The objectives of the study will be;

• To understand the concept of the interactional aerodynamics and computational aeroacoustics.
• To find out the impacts of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform.
• To explore the design of aerodynamic optimization of proprotors for the convertible rotor.
• To evaluate the optimization of the aerodynamic shape of a proporptor and its validation utilizing CFD and other experiments.
• To examine the optimization of the aerodynamic shape of tiltrotor blades equipped with the continuous morphing aerofoils.
• To find out the economic cost involved in the understanding of the effect of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform.
• To do the critical review on analysing the impacts of interactional aerodynamics on computational aeroacoustics.
• To assess the positive and negative effects of interactional aerodynamics on computational aeroacoustics.
• To explore the strategies involved in understanding the impacts of interactional aerodynamics on computational aeroacoustics.
• To compare the past and current approaches that can be employed to examine the impacts of interactional aerodynamics on computational aeroacoustics of Lockheed Martin’s X2 platform.

Aim of the study The aim of the study will be “To do the critical analysis of digital control law synthesis for Lockheed Martin’s innovative control effectors aircraft concept. Can this technology set the fundamentals for 6th generation fighter jets?”

Objectives of the study The objectives of the study will be;

• To understand the concept of digital control law synthesis.
• To understand the impacts of the technology for the 6 th generation fighter jets.
• To explore the applications of digital control law synthesis for the 6th generation fighter jets.
• To compare the technologies used in the past years with the applications of digital control law synthesis.
• To set the scope and design requirements for the performance analysis to categorize the aircraft.
• To examine the conventional and modern flight control system design process for the tailless aircraft Simulink model with innovative control effectors provided by Lockheed Martin
• To evaluate open-loop dynamics revealed modal instabilities as well as state and control coupling.
• To find out which method will achieve the stable augmented control of the innovative control effectors (ICE) aircraft throughout the flight envelope.
• To understand the tailless fighter aircraft model for control-related research and development.

Aims: Several experiments have been performed on aerodynamic load models with defined parameters to evaluate the critical decreased dry- and ice-galloping velocity of a conductor at a given wind-related yaw angle of the conductor. However, the researcher observed that there is not a vast amount of research in the domain of mitigating the outer structural and signal structures by using aerodynamic load identification. Therefore, the researcher wants to fill this gap. The aim outlined by the researcher for carrying out this research is to study the aerodynamic load identification and prediction of wind induced vibration on the outer structural and signal structures, in order to minimize them. In this context, the researcher considers Antonov 225 aircraft so that research outcomes can be meet in an effective manner. Objectives: In order to endorse the primary objective of the research study, the researcher formulated the secondary objectives so that the potential outcomes of the study can be met in an effective manner. Following are the secondary objective of the study are as following:

• To study the significance of aerodynamic load identification in Antonov 225 from theoretical perspective.
• To critically analyze the aerodynamic load identification and prediction of wind induced vibration on the outer structural and signal structures.
• To examine the impact of aerodynamic load identification for minimizing the wind induced vibration on the outer structural and signal structures.
• To identify the potential factors affecting wind induced vibration on the outer structural and signal structures.
• To investigate the implications of using aerodynamic load identification in Antonov 225 for diminishing the wind induced vibration on the outer structural and signal structures.

In recent decades, the accretion of ice on aircraft or wind turbines has been generally recognised as a significant safety hazard. Therefore, the researcher wants to perform a research study in this domain. The purpose for conducting this research study is to perform an experimental investigation on thermodynamic characteristics of dielectric barrier discharge (DBD) plasma and its applications for aircraft icing mitigation. In this regard, the researcher takes specific note of the case of the Air Bus A-380 in order to support the main goal of the study being carried out.

The researcher designs the secondary objectives by narrowing down the primary objective into sub-parts in order to support the primary purpose of the study. Following are the secondary objectives:

• To investigate the implications of dielectric barrier discharge (DBD) plasma from theoretical perspective.
• To evaluate the approaches for icing control by using dielectric barrier discharge (DBD) plasma.
• To perform an experimental study on Air Bus A-380 to bestow more reliable and safe solutions to mitigate aircraft icing.
• To examine thermodynamic characteristics of dielectric barrier discharge (DBD) plasma and its applications for aircraft icing mitigation.
• To provide relevant recommendations to effectively utilizing the thermodynamic features of dielectric barrier discharge (DBD) plasma for aircraft icing mitigation.

The speed of commercial aircraft has been limited for decades by the sound barrier. However, recent noticeable increases in air travel and the acknowledgement of time as a desirable commodity for travelers have called for quicker, more efficient commercial transport. Therefore, the researcher wants to conduct the research study in the domain of aerospace by specifically considering supersonic transport design. The aim of researcher in this study is to perform a critical study on reducing the dimensionality of a commercial supersonic transport design space by using active subspaces. In this context, the researcher wants to make use of air freight to minimize reliance on sea freight transport.

The researcher has developed secondary objectives in order to support the main objectives of the research, which are as follows:

• To comprehend the implications of using active subspaces for reducing dimensionality of a commercial supersonic transport design.
• To critically analyze the impacts of using active subspaces air freight for decreasing dependency on sea freight transport.
• To build a framework for commercial supersonic architecture that involves active subspace surrogates to enhance the exploration of design space.
• To provide adequate recommendations on effectively using active subspaces air freight for reducing the dependency on sea freight transport.

The aim or carrying out this research study is to critically evaluate the supersonic boundary layers over an adiabatic wall with deformations. In this regard, the researcher wants to analyze the use of supersonic boundary layers for bringing back supersonic passenger airliners in future.

T he primary of this research study is to evaluate the supersonic boundary layers over an adiabatic wall with deformations. Moreover, the researcher is inclined to explore the underlying factors which can guarantee the performance of the forthcoming supersonic passenger airliners. For the purpose of supporting the primary objectives of the research, the researcher formulated secondary objectives which are as following:

• To investigate the implications of supersonic boundary layers over an adiabatic wall encompassing deformations.
• To critically evaluate which aspects of supersonic boundary layers can be beneficial over an adiabatic wall to bring back supersonic passenger airliners in near future.
• To explore which factors could guarantee the performance of the forthcoming supersonic passenger airliners.
• To investigate prospective passengers' views of supersonic transport as a potential future mode of transportation.
• To provide appropriate recommendations on successfully using supersonic boundary layers for bringing back supersonic passenger airliners in future.

For modern engineered systems like unmanned aerial systems and turbomachinery, the design of aerodynamic surfaces is essential. Therefore, the researcher wants to explore the multi-objective aerodynamic design by using different methods and techniques.  In order to conduct this research study, the researcher has formulated the key aim, which is to perform a systematic study on exploring multi-objective aerodynamic design. The researcher is inclined to explore the multi-objective aerodynamic design using multi-fidelity methods and novel pareto set identification techniques.

The primary objective of this research is to fill the knowledge gap and explore alternatives for multi-objective aerodynamic architecture experimentation that are useful in multi-fidelity. In order to foster the primary objective of the research project, the secondary goal is designed by the researcher to enable the future findings of the study to be reached effectively. The secondary of the study are as following:

• To study the concept of aerodynamic design from theoretical perspective.
• To explore multi-objective aerodynamic design using multi-fidelity methods.
• To investigate novel pareto set identification techniques that aligns with multi-objective aerodynamic design.
• To assess the scalability of using the multi-fidelity methods and novel pareto set identification techniques.
• To achieve optimized solutions which are non-commensurate using multi-fidelity techniques in the vicinity of a design configuration.

Aerospace Engineering Dissertation Ideas For Staggering Dissertations

Aerospace engineering is a very vast and innovative field. Therefore, aerospace engineering dissertation ideas will prove to be more helpful for you which you can customize into your favourite topic, rather than a handful of aerospace engineering dissertation topics. For this reason our market specialist senior expert writers have also prepared a free list of the best aerospace engineering dissertation ideas that you can use to custom make aerospace engineering dissertation topics for yourselves.

The aim of the study is to conduct a critical analysis of the lag parameter method for the modelling of turbulence of general and common air route taken by airline passenger to make themselves safe. Therefore, the research aims to identify the factors of service quality in the airline industry.

The primary objective of the study is to achieve the aim of the study. However, the primary objective of the study can be achieved through various secondary objectives. Therefore, the secondary objectives of the study are:

• To determine the procedures and methods that the airline must follow in order to offer safe and secure air travel.
• To evaluate how the service quality of airline can be improved.
• To evaluate the association between the profitability of airline and the service quality.

The aim of the study is to conduct an experimental analysis on the de-icing/anti-de-icing technology and the icing physics of wind turbine. The research aims to analyze which approach is cost-efficient for the aircraft who are flying at enormously high altitudes. Therefore, the research aims to explain the physics pertinent of icing toward wind turbines. Furthermore, the research aims to suggest robust and effective mitigation strategies of ice for the wind turbines.

• To measure the process of active ice accretion over the blade surfaces of the wind turbine.
• To analyze the ice accreting blades’ aerodynamic penalties.
• To promote and encourage a fine understanding regarding the transfer of heat during the process of icing.
• To suggest mitigation strategies of ice for the wind turbine blade.
• To analyze the effectiveness, flexibility, central control and mass-production possibilities, economical efficiencies and safety of the proposed suggestions.
• To evaluate which approach is cost-efficient for high altitude flying of aircraft.

The aim of the study is to conduct a critical exploratory analysis to determine the bio-inspired surface coating for the icing mitigation of aircraft. The research aims to study that can the nanotechnology be the everlasting solution for the icing problem of the surface.

Objectives :

• To develop a wind tunnel which will thereby quicken the droplets of water and determine the impact of highspeed droplet on the dynamics and coating of the bio-inspired surface.
• To establish an accelerated and smooth spray generator to illustrate the bio-inspired surface durability.
• To measure and quantify the details of the flow of the droplets which are wind-drive and to develop a theoretical model for forecasting the motion of wind-driven droplet on the different surface coating which are bio-inspired.
• To offer a suggestion for the promising coating selection for icing mitigation of aircraft.

The aim of the study is to conduct a dynamic analysis of the complex wind turbine blade. The research aims to study the effectiveness of these composite blade. Furthermore, the aim of the study is to evaluate how much long-lasting, sturdier and stronger these blades areas compare to old ones. Therefore, the purpose of the study is to develop a basis for analyzing the level of accuracy required in the prediction model of load by comparing the wind turbine blade composite material results for the experimental wind loads set. Additionally, the research aims to evaluate how the wind forecasting dynamics can be enhanced for reliable, economical and safe operations of the wind turbines. The research will study the procedure of blade modelling, aerodynamic load calculations form the wind data collection and the analysis of fatigue for the wind turbine blade.

• To study complex blades of wind turbines.
• To evaluate the effectiveness of each blade.
• To analyze as compare to conventional blades, how stronger these blades are?

The aim of the study is to study the electrical vertical landing and takeoff (VTOL) aircraft management in urban air mobility which are on-demand. The study aims to develop the most energy effective arrival trajectory with battery endurance that is limited, eVTOL type and the particular CONOP (Concept of operation). The research aims to meet the allocated RTA constraint with secure eVTOL separation requirement of aircraft and partial vertiport time slot of arrival.

• To study the scheduling of eVTOLs and the sequence of arrival.
• To solve and formulate the scheduling problem and sequencing for assorted eVTOLs fleet in order to enable efficient and safe UAM operations.

The aim of the study is to evaluate the effectiveness of the airline system in offering medical help to people in the urban hub cities which are overpopulated. Therefore, the research emphasizes on the urban development central aspect that is urban form and transport and studies how these two will certainly shape the provision of goods and services, access to people and the information in cities.

• To evaluate the effectiveness of airline in offering medical support.
• To investigate the association between passenger loyalty, passenger satisfaction and the service quality of the airline.
• To determine factors which contribute to the service quality of airlines.

The aim of the study is to understand the requirement of technological development for the assessment and valuation in the space habitat making. Therefore, the study aims to fill the current gaps in technology selection and subsystem sizing. The aim of the study is to develop a methodology to size dynamically subsystems of space habitats and choose technologies to carry various missions.

• To evaluate the requirement of technological advancement for the development of space habitats.
• To analyze how the subsystem can be size dynamically and chose for various missions.
• To evaluate the challenges of space exploration.
• To analyze the space habitats characteristics.

The aim of the study is to conduct a critical exploration and the analysis of the performance of the techniques for the optimization of supersonic descent production aerodynamics. The study aims to analyze how this technique will certainly support and assist in manned landing on the surface of Mars.

• To evaluate the performance of the novel techniques in the optimization of supersonic descent production aerodynamics.
• To analyze the effectiveness of these techniques.
• To study how these technologies will certainly help in manned landing on the surface of Mars.

The aim of the study is to conduct a novel approach on how the algorithms of deep learning can be implemented for enhancing the attitude of spacecraft and orbit control system (AOCS).

• To explore the deep learning application on the isolation and fault detection in the AOCS.
• To establish a framework for additional research for the aerospace deep learning.
• To create or acquire the important telemetry that is to be used for testing and training the classifiers of AOCS.
• To develop a model of simulation which is certainly capable of the simulation of on-orbit faults.
• To analyze the basis of spacecraft attitude control and determination.

Aims and objectives

The aim of this study is that to critically evaluate the using of large eddy simulation and the machine learning augmentation for flow over bumps enabled turbulence modelling in the space crafts. However, large eddy simulation is the mathematical model which used the computational fluid dynamics for turbulence. The turbulent flow with two-dimensional bumps by the well resolved large eddy simulation. The data augmentation also reduces overfitting when training a machine learning. This is also closely related to the oversampling in data analysis. The optimization method is used to extract fields of variables used in the turbulence closure models.

            The objectives of this study are the following:

• To critically analyse the large eddy simulation LES and data augmentation.
• To analyse the turbulence modelling in space crafts.
• To evaluate the large eddy simulation and machine learning augmentation for flow over bumps enabled turbulence modelling in space crafts.

Aims The aim of this study is that it is the novel approach use of the hybrid electric distributed propulsion for landing and vertical take-off of the space crafts. This is the study also analyse the effectiveness of this system for the atmosphere in entering and leaving in different planets. This research also explores the interaction between the hybrid electric power system (HEPS) and aerodynamics and control for vertical take-off and landing (VTOL) aircraft applications with the selection of the configuration for evaluation of interaction with the hybrid power system. Objectives The objectives of this study are the following:

• To analyse the Hybrid electric power system (HEPS) and vertical take-off and landing (VTOL).
• To assess the novel approach or idea of using hybrid electric distributed propulsion for vertical takeoff and landing spacecraft.
• To assess the system's affectivity for entering and leaving the atmosphere of different planets.
• To analyse the impact of hybrid electric distributed propulsion for vertical take-off and landing spacecraft and atmosphere on other planets.

Consult Our Writers to Discuss Your Needs

View different varieties of dissertation topics and samples on multiple subjects for every educational level

A few pointer to make your dissertation topics more attractive are that you should make them compelling by using flashy and witty words that instantly capture a reader’s attention. You should also make your topics a bit informative to reveal the central idea behind your dissertation and lastly you should also make them indicative.

Your dissertation’s tone should be formal but yet creative. Your dissertation should be properly structured into chapters and sub chapters. You should be careful about plagiarism, try to keep it as low as possible and lastly hire a professional editor once you are done with your dissertation.

You can find data for your dissertation from IA State, Ga Tech, W-Mich Edu, Research gate to name a few.

The wordcount for your dissertation depends on a number of things e.g. your level of degree, your topics, the type of research involved. And the word count ranges from anywhere in between 10000 to 80000 words.

Home > Research > Student Research > Graduate Research > Master’s Theses > Aerospace Engineering

• Aerospace Engineering

Theses/Project Reports from 2024 2024

A Comparison Of Western And Eastern Soft Systems Approaches , John L. Anaya, John L. Anaya, and John L. Anaya

Short Arc Initial Orbit Determination For Leo Objects And The Impact Of Observation Eelevation On Predictive Accuracy , Alexis DiGregorio

The Pressure Distribution Of Rotating Cylinders Using An Onboard Wireless Data Acquisition System , Nathan Eller

Automatic Mass Balancing Of A Spacecraft Attitude Dynamics Simulator With Six Sliding Masses , Amelia J. Gilman

The Effect Of Atomic Oxygen On Additively Manufactured Materials , Ryan Grogan

A Hardware-In-The-Loop Star Tracker Test Bed , Ashley Haraguchi

Exploring The Feasibility Of The Resonance Corridor Method For Post Mission Disposal Of High-LEO Constellations , Payton G. Porter

Supersonic Air Inlet Modeling Using the Method of Characteristics , Shay S. Takei

Preliminary Analysis Of A 12U Astronomy CubeSat , Charles Van Steenwyk

Theses/Project Reports from 2023 2023

Launch Vibration Attenuation For In-Space Assembly Cargo , Jered Bell

Development Of Load Measurement Technique For Arbitrary Shapes , Quintin J. Cockrell

Parametric Optimization Of A Wing-Fuselage System Using A Vorticity-Based Panel Solver , Chino Cruz

Structural Design, Modeling, And Analysis Of The Wing For A World Speed Record-Breaking Turbo-Prop Racing Airplane , Joseph C. Hammond

Gyroless Nanosatellite Attitude Determination Using an Array of Spatially Distributed Accelerometers , Kory J. Haydon

Refactoring Dependency Loading And Standardizing Factory Patterns In The Horizon Simulation Framework , Jack W. Kelly

Autonomous Attitude Consensus for Nanosatellite Formations in LEO , Laird J. Mendelson

Distributed Control of Servicing Satellite Fleet Using Horizon Simulation Framework , Scott Plantenga

Feasibility Assessment of an All-Electric, Narrow-Body Airliner , Ariel Sampson

Coupled Boundary Conditions for Modeling Airbreathing Engines , Adam Louis Waldemarson

Theses/Project Reports from 2022 2022

Testing and Verification for the Open Source Release of the Horizon Simulation FrameworTesting and Verification for the Open Source Release of the Horizon Simulation Framework , William J. Balfour

Project Management and Systems Engineering Framework for Educational Cubesat Missions , Bailey Garrett

The Effects of Atomic Oxygen on Silicone and Carbon-Based Contamination , Mayana W. Gordon

Method and Simulation of On-Orbit Sub-microthrust Evaluation , Jonathan Hood

Spacecraft Trajectory Optimization Suite: Fly-Bys with Impulsive Thrust Engines (Stops-Flite) , Aaron H. Li

Development of a Dual-Band Radio Repeater to Be Carried by a Fixed-Wing Small Unmanned Aerial System , Carl Recine

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Aerospace engineering articles from across Nature Portfolio

Aerospace engineering is the branch of engineering that designs and builds machines for flight. This includes craft used both inside (aeronautical engineering) and outside (astronautical engineering) the Earth’s atmosphere. Aerospace engineering combines an understanding of fluid dynamics, robust but lightweight materials and the chemistry and thermodynamics of engines.

Latest Research and Reviews

Efficient deep reinforcement learning based task scheduler in multi cloud environment

• Sudheer Mangalampalli
• Ganesh Reddy Karri
• Barno Sayfutdinovna Abdullaeva

Seasonal and geographic viability of high altitude balloon navigation

• David Brown
• Marianna Linz
• Jared Leidich

An adaptive operation planning and EBO-BPNN optimization method for decision support systems

• Yunxiao Liu
• Yiming Wang
• Jianliang Ai

Robust quantitative X-ray phase diagnostic for carbon composite characterisation in the context of lightning induced risk

• Laureen Guitard
• Adrien Stolidi
• Amelie Jarnac

The oxidation behavior and interfacial reaction between SiO 2 coating and Ti45Al8.5Nb alloy

• Liang-Liang Wu
• Hao-Jie Yan

Neural network optimal control for tripartite UAV confrontation systems based on fuzzy differential game

• Xingjian Fu

News and Comment

Emerging photovoltaics for onboard space applications.

Thin-film solar cells are promising for providing cost-effective and reliable power in space, especially in multi-junction applications. To enhance efficiency, robustness and integration, advancements at the cell level must be combined with improvements in assembly and panel design. Ensuring that solar cells can provide sustained performance is also essential for minimizing space debris.

• Anita Wing Yi Ho-Baillie
• Stephen Bremner

Ultralightweight perovskite solar cells for use in drones

Ultralightweight perovskite solar cells that achieve a specific power of up to 44 W g –1 and good stability are developed through engineering of the photoactive layer and substrate. These solar cells can be integrated into a drone to enable energy-autonomous flight.

Design and microstructuring of materials to boost spacecraft ion propulsion

As new materials and manufacturing techniques are discovered, their benefits transform every branch of science and engineering. In spacecraft propulsion, a new generation of ion engines could provide unprecedented performance and flexibility in space mission design.

• Paulo C. Lozano

Domains of life sciences in spacefaring: what, where, and how to get involved

The integration of biology and spacefaring has led to the development of three interrelated fields: Astrobiology, Bioastronautics, and Space Bioprocess Engineering. Astrobiology is concerned with the study of the origin, evolution, distribution, and future of life in the universe, while Bioastronautics focuses on the effects of spaceflight on biological systems, including human physiology and psychology. Space Bioprocess Engineering, on the other hand, deals with the design, deployment, and management of biotechnology for human exploration. This paper highlights the unique contributions of each field and outlines opportunities for biologists to engage in these exciting avenues of research. By providing a clear overview of the major fields of biology and spacefaring, this paper serves as a valuable resource for scientists and researchers interested in exploring the integration of these disciplines.

• Aaron J. Berliner
• Spencer Zezulka
• Adam P. Arkin

Propelling the widespread adoption of large-scale 3D printing

3D printing can be used to automate the manufacturing of building elements for large-scale structures such as skyscrapers, aircraft, rockets and space bases without human intervention. However, challenges in materials, processes, printers and software control must first be overcome for large-scale 3D printing to be adopted for widespread applications.

• Wouter De Corte
• Viktor Mechtcherine

Europe’s Ariane woes

With the retirement of Ariane 5, Europe lost its only heavy-lift rocket — one that carried most of ESA’s fleet of large astronomy missions. The long-term future of independent access to space for Europe is not straightforward and can complicate the European space exploration roadmap.

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• farmacia-barato.com Levitra es un fármaco oral que toma para tratar la disfunción erectil.

Research topics

Research topics can be generally divided in two main areas:

• Aeronautics

I conduct research in the following lines of reaserch

• Low-Thrust trajectory optimization
• Flight Plan Optmization
• Conflict detection and resolution
• Robust flight planning
• Avoidance of storms
• Artificial Intelligence applied to Capacity-Demand balancing

An undergraduate introductory course to the fascinating discipline of aeronautical engineering.

Also available at:

Research Areas

Michigan Aerospace remains a leader in aerospace research and education, covering an expansive array of topics from unmanned air and space vehicles to commercial airliners. The ever-evolving topics in aerospace encompass the traditional areas of gas dynamics, flight dynamics, control, structures and materials while probing visions of future needs for the aerospace enterprise. Research in aerospace engineering brings our best together to solve tough problems.

Aerodynamics & Propulsion

Aerodynamics & Propulsion is important for numerous aspects of aerospace engineering, such as airplane aerodynamics, helicopter aerodynamics, jet propulsion, rocket propulsion, advanced propulsion, properties of the space environment, and many others.

Autonomous Systems & Control

The department has a long history of excellence in the areas of flight dynamics and control systems. It was one of the first engineering departments in the nation to offer courses in automatic control, flight dynamics, and simulation.

Computation

Computation plays a fundamental role in the design, analysis and operation of modern Aerospace systems. Applications include flight software, embedded computing for on-board control, optimization of structural, aerodynamic and propulsion systems, etc.

Model Based Systems Engineering Lab

The Model-Based Systems Engineering (MBSE) Lab provides forward thinking industry tools to fill some critical skills gaps between engineering graduates and industry requirements. Program projects undertake research that leverages digital modeling to improve operational and financial efficiencies in engineering design and development.

Space Systems

A subset of faculty members in Aerodynamics and Propulsion and Dynamics and Controls develop spacecraft and advanced spacecraft subsystems such as propulsion and control systems. Experimental and computational studies center around spacecraft electric propulsion (EP) systems, such as Hall thrusters. 

Structures & Materials

Structural mechanics is the study of the mechanical behavior of solids and structures. This specialization covers theory, computations, experiments and implementation issues, as well as the study of specific cutting edge aerospace vehicles.

Sustainable Aviation

Sustainable aviation is a multi-disciplinary field that seeks solutions to improve the environmental and societal impacts of air transportation. This specialization covers highly efficient aircraft designs, novel propulsion systems, green aircraft technologies, and energy-optimized flight operations to reduce aircraft energy consumption, noise, and emissions.

GET INVOLVED

Be a part of research that pushes the boundaries of aerospace engineering.

Mechanical and Aerospace Engineering

Thesis - mechanical and aerospace engineering, student thesis overview.

This overview will describe the thesis, why it is very important to your graduate study, what are the steps that you will need to do and when they should or must be done, how to find an advisor, and the resources that are available to help you along the way. In the following section, questions and answers are provided for some common questions.

A thesis is a "position or proposition that a person (as a candidate for scholastic honors) advances and offers to maintain by argument." and a document containing results of original research and especially supporting a specific view.

What is a Thesis?

The thesis is the most important part of your graduate education. While the course work lays the foundation by providing analytical methods and tools, it is the thesis that provides to you the opportunity to use this knowledge in a new, original and creative manner. During your thesis research you will be able to consolidate what you have already learned, and possibly extend this by further self-study, and to use this body of knowledge to attack a new problem. The thesis will hopefully be your crowning achievement of your graduate study, and will be your introduction to the community of scholars.

Choosing Your Topic and Advisor

The first step in the thesis process is choosing an advisor and a topic. While your formal thesis slots may be in the last 2 or 3 quarters at NPS, it is very important that you have a thesis advisor and topic chosen well before this, preferably a year or so before you plan to graduate. During the time between choosing an advisor/topic and the start of your thesis slots, you should meet regularly with your advisor and spend a few hours a week reading background material and thinking about the problem.

The method for choosing your topic and advisor is completely up to you. However, you are strongly advised to talk to every faculty member in all the areas that you have any interest before making decisions. There are several questions you might want to ask yourself, before talking to the faculty. What type of work do you most enjoy? Generally, thesis research may be categorized as analytical (e.g. using a pencil and paper for mathematical modeling and derivation of solutions), computational (e.g. using finite element technique or computational fluid mechanics to find solutions), experimental (e.g. designing, building, or modifying an existing set-up to obtain new data) or some combination of the three. It is generally advisable that you take a course from a professor before you make a commitment to work for him or her. The Mechanical Engineering Faculty periodically schedule thesis opportunity presentations, where they will discuss their current research interests and the available topics. In addition, there is a ME website which contains short written descriptions for current thesis topics of ME faculty. You may talk to fellow students, who are close to graduating to discuss what they have done and how they enjoyed their experience. However, they probably will not be as good a source of what the available research topics are as the faculty members, themselves. Finally, you may wish to review previous thesis, as well as conference and journal publications from the various faculty members.  After you find an advisor and agree on the topic, you are required to fill out a thesis approval form, which must be signed by the thesis advisor, the Academic Associate and the Chairman of the Mechanical Engineering Department.

Common Pitfalls and Advice

While your advisor will help you along the way and provide broad guidance and feedback, it is the responsibility of the student to be self-motivated and to initiate all of the steps. Do not expect your advisor to provide a detailed, step-by-step, road map for you. You should be independent and think through problems first, before asking your advisor. However, that does not in any way mean you should avoid meeting with your advisor. You should meet regularly with your advisor to discuss what you have done, what issues have arisen, how you plan to solve them, and what your next steps should be.

One common problem faced by researchers, is the failure to sufficiently limit the scope of their work. Being overly broad can lead to a lack of focus and prevent any contribution from being made. It may seem to you that your advisor has asked you to solve a problem that you consider trivial and your may be inclined to broaden the scope. Stay focused on the immediate problem. If you solve the problem then by all mean go on to a larger problem. But initially, stay focus on a narrow and well-defined problem.

Thesis Proposals

One way that you can help yourself is to write a short Thesis Proposal. It can be useful in helping to consolidate your understanding and focusing your future work. This may be written after you have been working on the problem for several months, have read dozens of articles and it may contain the following elements:

• Introduction to the problem. This describes the problem and why it is important.
• State of the art. Literature review and what is not known.
• Objectives. Your goals for the work. What would be the desired outcome(s). Be specific. Do not say "to better understand something".
• Proposed work. Very limited and specific.

For you to make an original contribution, it generally requires that you have an understanding of what is already known, by experts in your field. Therefore, one of the primary resources on which you will depend is the NPS library and the reference staff. While the world-wide-web is becoming an increasing source of information, and you should make use of it, there are many primary sources, such as books and journals, which are not available on the web. Most of the information on the web is not archival in nature - that is, it might not exist if a certain site is closed. One of the most valuable skills you should learn during your thesis is how to obtain and process information and how to synthesize new results from that original information.

After your research is complete you will be required to write and submit a thesis document. For many of you it will be the longest document that you have written. There are several sources available to help you in writing the document, including "How to Write a Thesis" by the Mechanical Engineering Department and several guidelines and templates available on the NPS web site.

Finally you are required to make an oral presentation of your thesis research to the faculty and students of the Mechanical Engineering Department. The presentation is approximately fifteen minutes with about a 5-minute question and answer period. A document on how to prepare and deliver this presentation is available from the Mechanical Engineering Department.

Common Questions and Answers

Please visit our Thesis Q&A page  to view common questions and answers regarding your Thesis.

• Aerospace Engineering

A field that’s out of this world

As an aerospace engineer, you’ll dive into the thrills of space travel and exploration, whether it's with rockets, cutting edge drones or unmanned vehicles. Plus, you'll venture into the world of futuristic ground vehicles like hovercrafts, hydrofoil ships and lightning fast trains. Get ready to rocket into an exhilarating future with an aerospace engineering degree.

Bachelor of Science Aerospace Engineering

Study the basic principles of aerodynamics, solid mechanics and structures, stability and control, thermal sciences and propulsion. The curriculum consists of a combination of fundamentals, including mathematics and sciences, and practical laboratory experience which provides you access to modern engineering tools. Aeronautical engineering subjects are to be the focus of the discipline along with significant exposure to space-related topics.

Experiential Learning

Design, Build, Fly (DBF)

Bringing WVU students from all majors together to design, fabricate, and fly unmanned, electric-powered, radio-controlled aircraft (UAVs) which can best meet the specified mission profile set forth by The American Institute of Aeronautics and Astronautics (AIAA) DBF Committee. You will learn skills to accomplish various tasks that allow us to travel to and compete in the annual AIAA DBF Competition held in the Spring.

WVU MICROGRAVITY

Join the efforts of clubs like Microgravity, where you will conduct research and work collaboratively to develop a setting where functional 3D printing can co-exist in a reduced gravity environment.

Robotics Club

This student-run organization is dedicated to bring you into a diverse thinking group of students from all majors and develop skills to help each other grow in knowledge and community centered around robotics.

Materials Advantage & Materials Research Society (MA/MRS)

The WVU chapters of Material Advantage and Materials Research Society work together to build awareness and interest in materials science. Throughout the year, you will participate in various outreach programs and travel to materials related events and venues. Come to our next meeting to learn more about us and our activities.

American Institute of Aeronautics and Astronautics (AIAA)

AIAA is open to all students interested in aerospace engineering. You will attend guest seminars on aerospace engineering topics as well as field trips to an aerospace industry locations. AIAA meets monthly to discuss aerospace topics, fundraising ideas, and community service. We also organize at least one trip per school year to places like museums, air shows, or camping.

Formula SAE

West Virginia University Mountaineer Racing give you the opportunity to design and build highly competitive Formula SAE® race cars while preparing you to be the next generation of transformative engineers and business leaders for the automotive industry and related fields.

Designing rockets that reach for the stars

During in the 2022 Spaceport America Cup, West Virginia University’s Experimental Rocketry team was highly successful, earning 1st place in the 30,000 foot Student Researched and Designed Solid Fueled category and 2nd in the SDL Payload competition. This achievement marked the team's first successful 30,000 foot competition flight, as well as its first fully functional scientific payload deployment.

Focus Areas

Aerodynamics.

Predict and analyze the forces and resulting motion generated by the flow of air, water and other fluids around solid objects to aid in the creation of automobiles and weapon systems.

GUIDANCE AND CONTROL

Create software for flight control, including navigation and closed-loop feedback systems that allow users to maintain aerodynamic stability while guiding and maneuvering aircraft through a broad range of flight conditions.

SPACE FLIGHT SYSTEMS

Design various spacecrafts based on mission profiles from lift-off to re-entry, taking various mission objectives, communication protocols and management issues into consideration.

Be immersed in a variety of systems used to generate thrust for different types of airborne, waterborne and space vehicles, like air-breathing jet engines, gas thrusters and engines for launch vehicles and weapons systems.

STRUCTURES AND MATERIALS

Rely on numerical and structural analysis software, characterization facilities and their knowledge of material science to minimize the structural weight of aircraft, watercraft and space vehicles without degrading their strength and durability.

Undergraduate Research

Undergraduate research is a great way for you to gain experiential learning to stand out from the crowd in the workforce or build a portfolio for graduate studies. Aerospace engineering students have many areas to explore.

Nature of Program

Aerospace travel, space exploration, and flight of manned or unmanned vehicles continue to gain significance. In aerospace engineering, you'll get involved with the science and technology of advanced vehicles, including aircraft, rockets, missiles, and spacecraft. Although a specialized branch of engineering, it is also diverse. Aerospace technology has expanded to include design and development of earthbound vehicles such as ground-effect machines, hydrofoil ships, and high-speed rail-type systems. Combining the fundamentals — mathematics, sciences, and practical laboratory experience — you will have access to state-of-the-art labs and modern engineering tools to focus on aeronautical engineering subjects with significant exposure to space-related topics. 

In aerospace engineering students focus on the disciplines encountered in the design of aerospace vehicles, missiles, rockets, and spacecraft.  Study the basic principles of aerodynamics, solid mechanics and structures, stability and control, thermal sciences, and propulsion and participate in senior capstones in flight vehicle design course providing an experiential learning opportunity.

Real research for real problems

Amina wanted to conduct real research in cutting-edge labs — and she’s doing that and more at WVU. She’s a mechanical and aerospace engineering student working alongside award-winning faculty mentors and leading her peers in student government.

Individuals with aerospace engineering degrees have a global net to cast when looking for employment in their field. These are just some of the companies and government agencies that have recently hired our graduates:

Northrup Grumman, American Airlines, Boeing, Aurora, Eaton, U.S. Navy, First Energy, Fiat, Kraft, Toyota, NASA, Ford and NAVSEA

Meet one of our students who has gained experience in the workforce.

Paislee Adlington

Paislee Adlington, a dual mechanical and aerospace engineering student, created a path of success through her involvement in student organizations — Society of Women Engineers, WVU experimental rocketry club and amateur radio club — that lead her to create new passions and pursue new areas in engineering. Her drive and focus landed her an internship with Aurora Flight Sciences.

The Future Will Be Built By Those Who Are Willing To Go After It.

For more information about the aerospace engineering program, contact Jason Gross by email [email protected] or by phone 304-293-3111 .

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Browse dissertations / theses on a wide variety of disciplines and organise your bibliography correctly.

Figueroa, Leonard J. "Aerospace Intrapreneurship: Systems Engineering an Aerospace Front End." Digital Commons at Loyola Marymount University and Loyola Law School, 2017. https://digitalcommons.lmu.edu/etd/394.

Clark, Thomas William. "Aerospace power converter interfaces." Thesis, University of Manchester, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.514425.

Jenett, Benjamin (Benjamin Eric). "Digital material aerospace structures." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/101837.

Ashworth, Geoffrey (Geoffrey John). "Architectural disruption in aerospace." Thesis, Massachusetts Institute of Technology, 2009. http://hdl.handle.net/1721.1/55202.

Gostic, William J. (William John) 1957. "Aerospace supply chain management." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/10000.

Pratt, Roger W. "Control problems in aerospace engineering." Thesis, Loughborough University, 1995. https://dspace.lboro.ac.uk/2134/27604.

Borman, Stephen. "Sensorless drives for aerospace applications." Thesis, University of Newcastle Upon Tyne, 2012. http://hdl.handle.net/10443/1447.

Delfa, G. L. a. "Aerospace composite materials in fire." Thesis, University of Newcastle Upon Tyne, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.519566.

Falco, James A. (James Anthony) 1955. "Offsets and the aerospace industry." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/10008.

Stimac, Andrew K. (Andrew Kenneth) 1977. "Precision navigation for aerospace applications." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/16676.

Bílek, Jan. "Aerospace - Futuristický kokpit moderního letounu." Master's thesis, Vysoké učení technické v Brně. Fakulta informačních technologií, 2010. http://www.nusl.cz/ntk/nusl-237164.

Brentari, Mirko. "Hybrid Control For Aerospace Systems." Doctoral thesis, Università degli studi di Trento, 2019. https://hdl.handle.net/11572/368808.

Brentari, Mirko. "Hybrid Control For Aerospace Systems." Doctoral thesis, University of Trento, 2019. http://eprints-phd.biblio.unitn.it/3666/2/PhDThesisMirkoBrentari.pdf.

Roth, Matthew Adrian. "Vortex lattice methods for aerospace design." Thesis, University of Bristol, 2016. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.720833.

Landahl, Olof. "Weather visualization for the aerospace industry." Thesis, Linköpings universitet, Institutionen för teknik och naturvetenskap, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-95274.

Aouf, Nabil. "Robust control techniques for aerospace vehicles." Thesis, McGill University, 2001. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=38145.

Progoulakis, Losif. "Heated tooling for aerospace composites manufacture." Thesis, University of Plymouth, 2004. http://hdl.handle.net/10026.1/1105.

Butters, Jonathan David. "Terminology recognition in the aerospace domain." Thesis, University of Sheffield, 2012. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.575750.

Barker, A. J. "Thin film sensors for aerospace applications." Thesis, Swansea University, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.636037.

Knight, Sylvia Frances. "Natural language processing for aerospace documentation." Thesis, University of Cambridge, 2001. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.621395.

Ebadan, Gracie E. "Laser welding of selected aerospace alloys." Thesis, Loughborough University, 1989. https://dspace.lboro.ac.uk/2134/7114.

Kirtley, Aaron L. (Aaron Lloyd) 1977. "Fostering innovation across aerospace supplier networks." Thesis, Massachusetts Institute of Technology, 2002. http://hdl.handle.net/1721.1/82696.

Ferre, Gregoire 1978. "IT management in the aerospace industry." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/27014.

Roman, Marco Antonio 1971. "Lean aerospace initiative electronic sector study." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/82680.

Spendley, Paul R. "Design allowables for composite aerospace structures." Thesis, University of Surrey, 2012. http://epubs.surrey.ac.uk/810072/.

Ameyugo, Gregorio. "Distributed propulsion and future aerospace technologies." Thesis, Cranfield University, 2007. http://dspace.lib.cranfield.ac.uk/handle/1826/10029.

RAJYALAKSHMI, P. S., and R. K. RAJANGAM. "FLIGHT INSTRUMENTATION TELEMETRY FOR AEROSPACE APPLICATION." International Foundation for Telemetering, 1986. http://hdl.handle.net/10150/615418.

Farinha, Marques Vitor Manuel. "Lead free solders for aerospace applications." Thesis, University of Oxford, 2010. http://ora.ox.ac.uk/objects/uuid:85707054-bc46-44f3-b9c6-9fd29358ad25.

Jönsson, Gustav. "Material selection for an aerospace component." Thesis, KTH, Lättkonstruktioner, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-198494.

Schäfer, Lukas Matthias. "Design of reliable aerospace system architecture." Thesis, University of Edinburgh, 2018. http://hdl.handle.net/1842/31391.

Yeremenko, Roman, and Valeri Badakh. "Public access data in aerospace industry." Thesis, ORT Publishing, 2019. http://er.nau.edu.ua:8080/handle/NAU/40228.

Hanuska, Alexander Robert Jr. "Thermal Characterization of Complex Aerospace Structures." Thesis, Virginia Tech, 1998. http://hdl.handle.net/10919/36617.

Hamad, Baran, and Markus Englund. "Improved Release Mechanisms for Aerospace Applications." Thesis, Uppsala universitet, Tillämpad mekanik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-448399.

Saotome, Tsuyoshi. "Transparent polymer nanocomposites for aerospace applications." Diss., Restricted to subscribing institutions, 2009. http://proquest.umi.com/pqdweb?did=1970611211&sid=54&Fmt=2&clientId=1564&RQT=309&VName=PQD.

Riva, Sephira. "Scandium metal processing for aerospace application." Thesis, Swansea University, 2018. https://cronfa.swan.ac.uk/Record/cronfa39867.

Frauenberger, Douglas H. "Lean transformation in aerospace assembly operations." Thesis, Massachusetts Institute of Technology, 2007. http://hdl.handle.net/1721.1/39728.

McQuarrie, Allan J. (Allan John) 1963. "Fire fighting in aerospace product development : a study of project capacity and resource planning in an aerospace enterprise." Thesis, Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/29535.

Liaghati, Amir, Nick Chang, Mahsa Liaghati, and John Blumer. "PREDICTIVE TELEMETRY MODELS FOR AEROSPACE FLIGHT MISSIONS." International Foundation for Telemetering, 2017. http://hdl.handle.net/10150/627017.

Strubel, Vincent. "Particle entrapment in EHD contacts - Aerospace applications." Thesis, Lyon, 2016. http://www.theses.fr/2016LYSEI098/document.

White, Caleb, and caleb white@rmit edu au. "Health Monitoring of Bonded Composite Aerospace Structures." RMIT University. Aerospace, Mechanical and Manufacturing Engineering, 2009. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20090602.142122.

Letovsky, Robert. "Public policy and the Quebec aerospace sector." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp02/NQ47721.pdf.

Levedahl, Blaine Alexander. "Decentralized Autonomous Control of Aerospace Vehicle Formations." NCSU, 2003. http://www.lib.ncsu.edu/theses/available/etd-03062003-104749/.

Marvasti, Mazda Alim. "Applications of fractal geometry in aerospace engineering." Diss., Georgia Institute of Technology, 1991. http://hdl.handle.net/1853/12079.

Lazim, Duraid. "Springback in draw-bending on aerospace alloys." Thesis, McGill University, 2003. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=79244.

Ma, Weitao. "Cost modelling for manufacturing of aerospace composites." Thesis, Cranfield University, 2011. http://dspace.lib.cranfield.ac.uk/handle/1826/6279.

Ashry, Mahmoud Mohamed. "Control of multivariable aerospace and industrial systems." Thesis, University of Manchester, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.504785.

Jaffery, Mujtaba Hussain. "Precision landing and testing of aerospace vehicles." Thesis, University of Surrey, 2012. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.551147.

Tuppen, S. J. "Resistance bonding of titanium based aerospace alloys." Thesis, Swansea University, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.639270.

Wechsler, Andrew Philip. "Improving fault tolerant drives for aerospace applications." Thesis, University of Newcastle Upon Tyne, 2013. http://hdl.handle.net/10443/1841.

Kudesia, Sean Swarup. "Precision Nd:YAG laser drilling of aerospace materials." Thesis, Heriot-Watt University, 2003. http://hdl.handle.net/10399/387.

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Willie Jones covers transportation for IEEE Spectrum and the history of technology for The Institute.

Wesley L. Harris [5th from left] poses with some of the MIT graduate students he advises in their pursuit of advanced degrees in aeronautics and astronautics.

Wesley L. Harris ’s life is a testament to the power of mentorship and determination. Harris, born in 1941 in Richmond, Virginia, grew up during the tumultuous years of the Civil Rights Movement and faced an environment fraught with challenges. His parents, both of whom only had a third-grade education, walked to Richmond from rural Virginia counties when the Great Depression left the region’s farming communities destitute. They found work as laborers in the city’s tobacco factories but pushed their son to pursue higher education so he could live a better life.

Today, Harris is a professor of aeronautics and astronautics at MIT and heads the school’s Hypersonic Research Laboratory . More importantly, he is committed to fostering the next generation of engineers, particularly students of color.

“I’ve been keeping my head down, working with students of color—especially at the Ph.D. level—to produce more scholars,” Harris says. “I do feel good about that.”

From physics to aerospace engineering

Harris’s journey into the world of science began under the guidance of his physics teacher at the all-Black Armstrong High School , in Richmond. The instructor taught Harris how to build a cloud chamber to investigate the collision of alpha particles with water droplets. The chamber made it possible to visualize the passage of ionizing radiation emitted by radium 226 , which Harris sourced from a wristwatch that used the substance to make the watch hands glow in the dark.

The project won first prize at Virginia’s statewide Black high school science fair, and he took the bold step of signing up for a separate science fair held for the state’s White students. Harris’s project received the third-place prize in physics at that event.

Those awards and his teacher’s unwavering belief in Harris’s potential pushed him to aim higher. He says that he wanted nothing more than to become a physicist like her. Ironically, it was also her influence that led him to shift his career path from physics to aeronautical engineering.

When discussing which college he should attend, she spoke to him as though he were a soldier getting his marching orders. “Wesley, you will go to the University of Virginia [in Charlottesville],” she proclaimed.

Harris applied, knowing full well that the school did not allow Black students in the 1960s to pursue degrees in mathematics, physics, chemistry, English, economics, or political science.

The only available point of entry for him was the university’s School of Engineering. He chose aerospace as his focus—the only engineering discipline that interested him. Harris became one of only seven Black students on a campus with 4,000 undergrads and the first Black student to join the prestigious Jefferson Society literary and debate club. He graduated in 1964 with a bachelor’s degree in aerospace engineering. He went on to earn his master’s and doctoral degrees in aerospace engineering from Princeton in 1966 and 1968, respectively.

Harris’s Ph.D. thesis advisor at Princeton reinforced the values of mentorship and leadership instilled by his high school teacher, urging Harris to focus not only on his research but on how he could uplift others.

Harris began his teaching career by breaking down barriers at the University of Virginia in 1968. He was the first Black person in the school’s history to be offered a tenured faculty position. He was also the university’s first Black engineering professor. In 1972, he joined MIT as a professor of aeronautics and astronautics.

Harris’s dedication to supporting underrepresented minority groups at MIT began early in his tenure. In 1975, he founded the Office of Minority Education , where he pioneered innovative teaching methods such as videotaping and replaying lectures, which helped countless students succeed. “Some of those old videotapes may still be around,” he says, laughing.

“I’ve been keeping my head down, working with students of color—especially at the Ph.D. level—to produce more scholars. I do feel good about that.”

Over the years, he has periodically stepped away from MIT to take on other roles, including Program Manager in the Fluid and Thermal Physics Office and as manager of Computational Methods at NASA ’s headquarters in Washington, D.C., from 1979 to 1980. He returned to NASA in 1993 and served as Associate Administrator for Aeronautics, overseeing personnel, programs, and facilities until 1995.

He also served as Chief Administrative Officer and Vice President at the University of Tennessee Space Institute in Knoxville from 1990 to 1993 and as Dean of Engineering at the University of Connecticut , in Storrs, from 1985 to 1990.

He was selected for membership in an oversight group convened by the U.S. House of Representatives Science Subcommittee on Research and Technology to monitor the funding activities of the National Science Foundation . He has also been a member and chair of the U.S. Army Science Board .

Solving problems with aircraft

Harris is a respected aeronautical innovator. Near the end of the Vietnam War , the U.S. Army approached MIT to help it solve a problem. Helicopters were being shot down by the enemy, who had learned to distinguish attack helicopters from those used for performing reconnaissance or transporting personnel and cargo by the noise they made. The Army needed a solution that would reduce the helicopters’ acoustic signatures without compromising performance. Harris and his aeronautics team at MIT delivered that technology. In January 1978, they presented a lab report detailing their findings to the U.S. Department of Defense. “ Experimental and Theoretical Studies on Model Helicopter Rotor Noise ” was subsequently published in The Journal of Sound and Vibration . A year later, Harris and his colleagues at the Fluid Dynamic Research Laboratory wrote another lab report on the topic, “ Parametric Studies of Model Helicopter Blade Slap and Rotational Noise .”

Harris has also heightened scientists’ understanding of the climate-altering effects of shock waves propagating upward from aircraft flying at supersonic speeds. He discovered that these high-speed airflows trigger chemical reactions among the carbon, oxides, nitrides, and sulfides in the atmosphere.

For these and other contributions to aerospace engineering, Harris, a member of the American Institute of Aeronautics and Astronautics , was elected in 1995 to the National Academy of Engineering . In 2022, he was named the academy’s vice president.

A model of educational leadership

Despite his technical achievements, Harris says his greatest fulfillment comes from mentoring students. He takes immense pride in the four students who recently earned doctorates in hypersonics under his guidance, especially a Black woman who graduated this year.

Harris’s commitment to nurturing young talent extends beyond his graduate students. For more than two decades, he has served as a housemaster at MIT’s New House residence hall, where he helps first-year undergraduate students successfully transition to campus life.

“You must provide an environment that fosters the total development of the student, not just mastery of physics, chemistry, math, and economics,” Harris says.

He takes great satisfaction in watching his students grow and succeed, knowing that he helped prepare them to make a positive impact on the world.

Reflecting on his career, Harris acknowledges the profound impact of the mentors who guided him. Their lessons continue to influence his work and his unwavering commitment to mentoring the next generation.

“I’ve always wanted to be like my high school teacher—a physicist who not only had deep knowledge of the scientific fundamentals but also compassion and love for Black folks,” he says.

Through his work, Harris has not only advanced the field of aerospace engineering but has also paved the way for future generations to soar.

• Wesley L. Harris - InfiniteMIT ›
• Wesley Harris elected vice president of National Academy of ... ›
• Wesley L. Harris - MIT AeroAstro ›

Willie Jones is an associate editor at IEEE Spectrum . In addition to editing and planning daily coverage, he manages several of Spectrum 's newsletters and contributes regularly to the monthly Big Picture section that appears in the print edition.

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