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June 25, 2008, 00:40 |
Momentum Source Value
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#1 |
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Hi all, could any body help me defining the momentum source value for my problem. i understand that
Momentum Source X Component = -C*(u-uspec) how could i come out with the value for "C" my domain is a compressor blade i did a calculation as follows Momentum source = -c*m(v2-V1) where C - 10e5 m - mass flow rate V2 - exit velocity from the blade V1 - inlet velocity to the blade will it work if not how should i specify to get the right velocity and pr raise across the blade |
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