TY - JOUR
T1 - Two dimensional rotor blade numerical analysis using ANSYS
AU - Anand, Shlok
AU - Shenoy, Satvik
AU - Srinivas, G.
N1 - Publisher Copyright:
© Published under licence by IOP Publishing Ltd.
Copyright:
Copyright 2020 Elsevier B.V., All rights reserved.
PY - 2020/12/22
Y1 - 2020/12/22
N2 - 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.
AB - 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.
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U2 - 10.1088/1742-6596/1706/1/012221
DO - 10.1088/1742-6596/1706/1/012221
M3 - Conference article
AN - SCOPUS:85098494877
SN - 1742-6588
VL - 1706
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
IS - 1
M1 - 012221
T2 - 1st International Conference on Advances in Physical Sciences and Materials 2020, ICAPSM 2020
Y2 - 13 August 2020 through 14 August 2020
ER -