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July 7, 2020, 18:37
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Total Pressure Calculation
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#1 |
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New Member
mekim
Join Date: Sep 2019
Posts: 21
Rep Power: 6  |
Dear all!
I would like to simulate air flow around a rotating blade with rpm=17188.7, Compressible, transonic flow, and just one blade with cyclic conditions by using OpenFOAM extend 4.0. Which mach number do we use for to calculate -inlet or outlet- total pressure? ( relative mach? or absolute mach? ) Formula: Pt=P( 1 + (gamma-1)*0.5*mach(?)^2 )^(gamma/(gamma-1)) Thanks for your help. |
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July 8, 2020, 04:46
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#2 |
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Senior Member
Santiago Lopez Castano
Join Date: Nov 2012
Posts: 354
Rep Power: 15 |
You kind of answering your own question there
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