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behruz June 9, 2013 15:15

blowing & suction control mechanism on airfoil
 
hi all
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.
Re=500000
attack angle=18
injection angle=90 (Perpendicular to injection face)
velocity inlet=1
injection velocity=0.5
is there any one help me to solve it?!
tahnks

rahul.avinash April 25, 2014 19:51

Hi Behruz

I'm trying to work on a similar project. can you tell me if you were able to solve the problem?

Thank you


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