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July 30, 2014, 03:31	Boundary Condition	#1
RAHUL RAMANUJAM New Member RAHUL R Join Date: Jul 2014 Posts: 1 Rep Power: 0	Hi, I need to compute the lift and drag coefficients of an airfoil for angle of attack varying from -180 to +180 degree at an interval of 1 degree and for Mach number from .1 to 1. Is there any procedure to automate the procedure ?? Thank you in advance...

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airfoil, angle of attack, boundary condition, udf

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