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Introduction:

In the field of aerospace engineering, gas turbine engines play a vital role in powering aircraft and generating electricity. The efficiency and performance of these engines heavily rely on the combustion process within the engine. Computational modeling has become an essential tool in understanding and optimizing combustion processes in gas turbine engines. This thesis aims to explore the use of computational modeling in analyzing and predicting combustion phenomena in gas turbine engines.

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 Basics of combustion in gas turbine engines
2.3 Computational modeling techniques in combustion
2.4 Previous studies on combustion in gas turbine engines
2.5 Combustion modeling software
2.6 Challenges in modeling combustion in gas turbine engines
2.7 Combustion instability in gas turbine engines
2.8 Emission control in gas turbine engines
2.9 Heat transfer analysis in gas turbine engines
2.10 Future trends in computational modeling of combustion

Chapter 3: Research Methodology
3.1 Selection of combustion model
3.2 Mesh generation techniques
3.3 Boundary conditions for simulation
3.4 Validation of computational model
3.5 Sensitivity analysis of parameters
3.6 Computational resources and software used
3.7 Data analysis methods
3.8 Experimental setup for validation

Chapter 4: Discussion of Findings
4.1 Analysis of combustion simulations
4.2 Comparison with experimental results
4.3 Sensitivity of operating conditions on combustion
4.4 Effect of combustion model on results
4.5 Heat transfer analysis findings
4.6 Emission predictions
4.7 Combustion instability analysis
4.8 Optimization of combustion performance

Chapter 5: Conclusion and Summary
5.1 Summary of research findings
5.2 Achievements of the study
5.3 Limitations of the study
5.4 Recommendations for future research
5.5 Conclusion

Thesis Overview:

Computational modeling of combustion in a gas turbine engine is a complex and challenging task that requires a multidisciplinary approach. This thesis aims to investigate the use of computational modeling techniques to analyze and predict the combustion process in gas turbine engines. The introduction provides background information on the importance of combustion in gas turbine engines and the motivation for the study. The literature review explores previous studies on combustion in gas turbine engines, computational modeling techniques, and challenges in the field.

The research methodology chapter discusses the selection of combustion model, mesh generation techniques, boundary conditions, validation methods, and data analysis procedures. The discussion of findings chapter presents the analysis of combustion simulations, comparison with experimental results, sensitivity analysis, heat transfer analysis, emission predictions, and optimization strategies. The conclusion and summary chapter summarizes the research findings, achievements, limitations, and provides recommendations for future research in the field of computational modeling of combustion in gas turbine engines.

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