Not able to start a Supersonic-Calculation
Hi,
I'm not able to start a supersonic-Calculation in FLUENT. Here the facts. Please check it! If there are any problems, please note me. thanks a lot!!! pressure_inlet: Gauge Total Pressure = 300000 Pa Initial Gauge Pressure = 0 Pa pressure_outlet: Gauge Pressure = 0 Pa Solver: Standard k-Omega-Model Steady Coupled Material: air - ideal gas cp = constant Therm. Cond. = constant Viscosity = sutherland thanks for your efforts |
Re: Not able to start a Supersonic-Calculation
Hi u put the static pressure in the place of Initial Gauge Pressure . For e.g For M2 For Po=295760 Pstatic is 37800 Pa.
Regards Prasatth |
Re: Not able to start a Supersonic-Calculation
Thanks Prasath,
How I can calculate the pressures at M = 2 ? |
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