Low pressure turbine is the last turbine stage in a gas turbine engine. As per research, LPT is quite heavy and is even up to one third of the total weight of the engine. A lighter and stiffer material is required to decrease the weight of the stage for better performance of the engine.
Computational Modal Analysis of a Low Pressure Turbine blade of Different Materials
Low pressure turbine is the last turbine stage in a gas turbine engine. As per research, LPT is quite heavy and is even up to one third of the total weight of the engine. A lighter and stiffer material is required to decrease the weight of the stage for better performance of the engine.
In this project, modal analysis of the specified low pressure turbine blade is done computationally, by comparing nickel base and titanium base materials.
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