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Introduction

The development of micro-scale gas turbine engines has gained significant interest in recent years due to their potential applications in unmanned aerial vehicles, portable power generators, and micro-scale vehicles. These engines offer high power-to-weight ratios, efficient operation, and low emissions, making them ideal for a wide range of applications. However, designing and developing a micro-scale gas turbine engine presents several challenges, including thermal management, aerodynamics, and material selection.

This thesis focuses on the design and development of a micro-scale gas turbine engine, with the aim of addressing these challenges and advancing the state-of-the-art in micro-scale propulsion systems. The research will involve a combination of computational modeling, experimental testing, and system integration to optimize the performance of the engine and demonstrate its feasibility for practical applications.

Chapter 1: Introduction
1.1 Introduction
1.2 Background of study
1.3 Problem Statement
1.4 Objective of study
1.5 Limitation of study
1.6 Scope of study
1.7 Significance of study
1.8 Structure of the Thesis
1.9 Definition of terms

Chapter 2: Literature Review
2.1 History of gas turbine engines
2.2 Micro-scale gas turbine engine applications
2.3 Thermal management in gas turbine engines
2.4 Aerodynamic design considerations
2.5 Material selection for high-temperature applications
2.6 Combustion systems in gas turbine engines
2.7 Control systems for micro-scale engines
2.8 Performance optimization techniques
2.9 Previous research on micro-scale gas turbine engines
2.10 Gaps in current knowledge and research opportunities

Chapter 3: System Design and Methodology
3.1 Engine configuration and components
3.2 Computational modeling and simulation
3.3 Experimental testing procedures
3.4 Data analysis and performance evaluation
3.5 System integration and testing
3.6 Optimization techniques
3.7 Risk assessment and mitigation strategies
3.8 Ethical considerations in research

Chapter 4: System Implementation
4.1 Component manufacturing and assembly
4.2 Control system design and implementation
4.3 Thermal management system development
4.4 Combustion system design and testing
4.5 Aerodynamic optimization techniques
4.6 Materials testing and characterization
4.7 Performance testing and validation
4.8 System integration and operational readiness

Chapter 5: Conclusion and Summary
5.1 Summary of research findings
5.2 Discussion of key results and implications
5.3 Recommendations for future research
5.4 Conclusion and final remarks

Overall, this thesis will contribute to the advancement of micro-scale gas turbine engine technology and provide valuable insights for researchers, engineers, and industry professionals working in the field of propulsion systems. By addressing the key challenges and limitations in the design and development process, this research aims to facilitate the widespread adoption of micro-scale gas turbine engines in various applications.

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