Simulation at Cruise Condition
 

Hello Everyone,

I am Mehedi, a new comer to the CFD field.
Currently I am doing one CFD project as my Masters thesis. In this project, I have to simulate an aircraft model at cruise condition. Since the considered altitude is 43000ft, pressure and temperature are 16326 pa and 217K. Now where should I define this pressure and temperature value? and How ??

I hope u won’t feel bother for this silly question. Thank you for your time