blowing & suction control mechanism on airfoil
i am working on a project that is " NUMERICAL STUDY OF BLOWING AND SUCTION CONTROL MECHANISM ON NACA 0012 AIR FOIL" i want to calculate CL and Cd.i use k-epsilon and k-omega method.but these parameter that i get from solving in FLUENT are far from their in journal.
injection angle=90 (Perpendicular to injection face)
is there any one help me to solve it?!
I'm trying to work on a similar project. can you tell me if you were able to solve the problem?
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