[solomedic]

I am doing flutter analysis of AGARD 445.6 wing. all physics has been developed and I am sure that all settings are correct. the only problem that I am getting is setting the pressure. I have a reference pressure in default domain>basic settings and a reference pressure in air as ideal gas so what these pressure signifies? which pressure is used to find density. for density we use absolute pressure which is sum of reference and static pressure? from where I will get static pressure?


lets sum up. I want to have a dynamic pressure of 4500 Pascals at .9 Mach using air as ideal gas so what pressures and temp should I use? Kindly reply this is very Important