blowing & suction control mechanism on airfoil

behruz · June 9, 2013, 15:15

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

June 9, 2013, 15:15	blowing & suction control mechanism on airfoil	#1
behruz New Member behrooz Join Date: Mar 2013 Posts: 24 Rep Power: 13	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

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April 25, 2014, 19:51		#2
rahul.avinash New Member Raul Join Date: Apr 2014 Posts: 1 Rep Power: 0	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