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Introduction

Gas turbine engines are widely used in various industries such as aviation, power generation, and marine propulsion due to their high efficiency and power-to-weight ratio. One critical component of a gas turbine engine is the turbine blade, which is subjected to high temperatures, high centrifugal forces, and aerodynamic loads. Failure of a turbine blade can lead to catastrophic engine failure, making it essential to accurately analyze and predict the mechanical behavior of the blade under different operating conditions.

Finite Element Analysis (FEA) has emerged as a powerful tool for the structural analysis of complex components such as turbine blades. FEA allows for detailed modeling of the geometry, material properties, and loading conditions of the blade, enabling engineers to simulate its behavior and assess its structural integrity. This thesis focuses on the application of FEA to analyze a turbine blade for a gas turbine engine, with the aim of improving the design and performance of the blade.

Table of Contents

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 Gas Turbine Engine Overview
2.2 Turbine Blade Design and Function
2.3 FEA in Gas Turbine Blade Analysis
2.4 Previous Studies on Turbine Blade Analysis
2.5 Material Modeling in FEA
2.6 Meshing Techniques in FEA
2.7 Boundary Conditions and Loading in FEA
2.8 Validation of FEA Results
2.9 Optimization of Turbine Blade Design
2.10 Future Trends in FEA for Turbine Blade Analysis

Chapter 3: Research Methodology
3.1 Selection of Turbine Blade Geometry
3.2 Material Properties and Modeling
3.3 CAD Modeling of Turbine Blade
3.4 Mesh Generation
3.5 Application of Boundary Conditions
3.6 Load Analysis
3.7 FEA Software Selection
3.8 Sensitivity Analysis
3.9 Validation Testing
3.10 Optimization Techniques

Chapter 4: Discussion of Findings
4.1 Static Analysis Results
4.2 Fatigue Analysis Results
4.3 Thermal Analysis Results
4.4 Modal Analysis Results
4.5 Failure Prediction and Analysis
4.6 Comparison with Experimental Data
4.7 Sensitivity Analysis Findings
4.8 Optimization Recommendations

Chapter 5: Conclusion and Summary
5.1 Summary of Findings
5.2 Contribution to Knowledge
5.3 Implications for Gas Turbine Blade Design
5.4 Limitations and Future Research Directions
5.5 Final Remarks

This thesis aims to provide a comprehensive analysis of a turbine blade for a gas turbine engine using Finite Element Analysis. By studying the structural behavior of the blade under various conditions, this research seeks to enhance the design and performance of turbine blades, ultimately improving the efficiency and reliability of gas turbine engines.

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