Two dimensional rotor blade numerical analysis using ANSYS

Document Type

Conference Proceeding

Publication Title

Journal of Physics: Conference Series

Abstract

Turbo-pump is an essential component in any rocket engine. The airfoil (NGTE 10C4 series) section of a rotor blade in the SSME (Space Shuttle Main Engine) was modelled along with a far-field of suitable shape and dimensions. The model was suitably discretized with proper amount of refinement, etc. A numerical simulation was then carried-out using ANSYS software with several iterations of varying inlet boundary conditions to check for any improvement in the performance of the rotor blade. Inlet velocity for optimum functionality of the blade was identified.

DOI

10.1088/1742-6596/1706/1/012221

Publication Date

12-22-2020

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