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Thermal Mechanical Analysis of High Pressure Turbine blade of a Turboshaft Engine
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Statistics
1Â Geometry
1Â Mesh
2Â Simulation setups
4Â Results
1Â Geometry 1Â Mesh 2Â Simulation setups 4Â ResultsAbout this project
Thermal Mechanical Analysis was carried on the HPT blade designed in DS Solidworks 2017. The loads were applied in 2 sections namely, (i) Mechanical loads in the form of centrifugal force and surface pressure on the leading edge of the blade, and (ii) thermal loads in the form of surface and convective heat flux. The support was kept as elastic to account for the micro displacements occurring due to extremely high temperatures of combustion gases inside of the gas generator of the engine.
