Solid Airfoil Analysi (Stagnation vs Static Temp) -- CFD Online Discussion Forums

April 26, 2009, 16:59	Solid Airfoil Analysi (Stagnation vs Static Temp)	#1
G. Gilson New Member G. Gilson Join Date: Apr 2009 Posts: 2 Rep Power: 0	Hi I am modelling a solid airfoil, usig ideal gas equation, mach number = 0.85, second order discretization, sutherland law (for viscosity), viscous heating on. Now I am interested in the temperatures inside the airfoil, and not on the surface. I am setting up a single boundary condition -pressure afar, with press =20980 and and angle of attack of 3 and a temp = 216.7 K. I am getting a result, stating that the inside temperature is = to the stagnant temperature. I have checked for grid independency, residuals and converge and all seems to be ok. Has anyone any idea, or come arcoss literature that might confirm my CFD analysis please?

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