Aerothermal Analysis of a Gas Turbine Blade

This study focuses on the aerothermal behavior and structural performance of gas turbine blades, essential for optimizing efficiency, durability, and thermal management in aerospace and power generation applications. Utilizing CFD (ANSYS Fluent) and FEA (ANSYS Static Structural), the project evaluates heat transfer, aerodynamic forces, and pressure distribution under extreme operational conditions.

Key Contributions & Results:

• Aerodynamic Optimization: Studied flow patterns, boundary layer behavior, and pressure gradients to improve blade efficiency and energy conversion.

• Thermal Stress Analysis: Identified hot spots and thermal fatigue regions, leading to improved cooling strategies and material selection.

• Structural Performance: Examined deformation and stress distribution, ensuring enhanced durability and resistance to high-temperature environments.

Industry Impact:

• Contributed to better gas turbine blade designs, improving fuel efficiency and operational lifespan.

• Provided validated simulation models to support next-generation aerospace propulsion systems.

• Advanced heat transfer management techniques, reducing thermal stresses and improving component reliability.