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AIAA 5th Drag prediction Workshop

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Old   June 13, 2014, 18:26
Default AIAA 5th Drag prediction Workshop
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Tarun Yadav
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Dear all,

I am doing simulations in Fluent using Spalart Allamaras for drag prediction of Common research model(NASA) at constant coefficient of lift 0.5, Mach number 0.85 and reference temperature is 100F. I am using pressure far field boudary and i am confused with the values of static pressure and temperature, can somebody tell?
Currently i am using 63177 Pa as static gauge pressure and 271.73 as temperature based on isentropic equation but i am not getting CL value 0.5 for 3 degree AOA.

Suggest me the correct values of temperature and presssure so that i can get CL value of 0.5.
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