airfoil incompressible BC implementation

October 12, 2006, 06:22

Does any one can help me with implementation of boundary condition in computational domain for incompressible flow about naca0012 airfoil. I'm using structured O-grid generation.

Thanks

October 16, 2006, 15:38

hi if you used vorticity-stream function formula the B.C of vorticity equation is zero on far-field, and on the body is calculatet from stream function equation. The B.c. of stream function is on body zero for no slip and on far-field is STRF=U*Y-V*X laith

October 12, 2006, 06:22	airfoil incompressible BC implementation	#1
Bounecer Guest Posts: n/a	Does any one can help me with implementation of boundary condition in computational domain for incompressible flow about naca0012 airfoil. I'm using structured O-grid generation. Thanks

October 16, 2006, 15:38	Re: airfoil incompressible BC implementation	#2
laith Guest Posts: n/a	hi if you used vorticity-stream function formula the B.C of vorticity equation is zero on far-field, and on the body is calculatet from stream function equation. The B.c. of stream function is on body zero for no slip and on far-field is STRF=UY-VX laith

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