Design and analysis of an electric aircraft propulsion system – Complete Phd and Masters Thesis

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Table of Contents

Chapter 1: Introduction
1.1 Background of the Study
1.2 Objective of the Study
1.3 Limitation of Study
1.4 Scope of Study

Chapter 2: Literature Review
2.1 History of Electric Aircraft Propulsion Systems
2.2 Benefits of Electric Aircraft Propulsion Systems
2.3 Challenges and Current Developments in the Field
2.4 Previous Studies on Electric Aircraft Propulsion Systems

Chapter 3: Research Methodology
3.1 Selection of Aircraft Configuration
3.2 Design of Electric Propulsion System Components
3.3 Analysis and Simulation Tools
3.4 Testing and Validation Methods

Chapter 4: Discussion of Findings
4.1 Performance Analysis of Electric Aircraft Propulsion System
4.2 Optimization of System Components
4.3 Comparison with Conventional Aircraft Propulsion Systems
4.4 Future Research Directions

Chapter 5: Conclusion and Summary
5.1 Summary of Key Findings
5.2 Implications of Research
5.3 Recommendations for Future Work
5.4 Conclusion

Thesis Overview

The “Design and Analysis of an Electric Aircraft Propulsion System” is a comprehensive study that aims to investigate the feasibility and performance of using electric propulsion systems in modern aircraft. The thesis is divided into five chapters, each focusing on different aspects of the research.

In Chapter 1, the introduction provides background information on the topic, sets out the objectives of the study, discusses the limitations of the research, and defines the scope of the study. Chapter 2 presents a thorough literature review, covering the history, benefits, challenges, and current developments in the field of electric aircraft propulsion systems.

Chapter 3 details the research methodology, including the selection of aircraft configuration, design of system components, analysis and simulation tools, and testing and validation methods. In Chapter 4, the findings of the study are discussed, including performance analysis, optimization of system components, comparison with conventional propulsion systems, and suggestions for future research.

Lastly, Chapter 5 offers a conclusion and summary of the thesis, highlighting key findings, implications of the research, recommendations for future work, and a final conclusion. Through this research, valuable insights into the design and analysis of electric aircraft propulsion systems will be gained, contributing to the advancement of sustainable aviation technologies.

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