need information regarding nozzle flow
hi, i am doing a nozzle flow analysis and i want to find out normal shock wave generated . can anybody help me in this regards
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Re: need information regarding nozzle flow
do the geometry mesh it
use wall (boundary condition) for walls pressure inlet for the inlet pressure oulet for the outlet get your values for Mach_0, total pressure and total temperature. use K-W turbulence model with compressible correction. have fun, regards, |
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