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rhoCentralFoam solver for simulating airfoil in high altitude

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Old   September 27, 2012, 12:22
Default rhoCentralFoam solver for simulating airfoil in high altitude
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I want to work with rhoCentralFoam solver for simulating airfoil in high altitude.
I change thermophysical property by using of us standard atmosphere 1976 for 70 km altitude. but I dont know what is the nmole,molweight and Hf properties in forward step--->constant--->thermophisicalproperty file.
thank you for your answering
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