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May 17, 2013, 03:48 |
Airfoil Validation
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#1 |
New Member
Manjunatha S
Join Date: Nov 2012
Location: Bangalore
Posts: 3
Rep Power: 14 |
I am simulating incompressible flow over NACA0012 airfoil using CFX. i used upwind scheme, SST turbulence model , Computational results are well matching with experimental results at low angles but i am not getting stall for any higher angles. can anybody please help me in this reg..
Thanks in Advance |
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May 21, 2013, 10:09 |
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#2 |
Senior Member
OJ
Join Date: Apr 2012
Location: United Kindom
Posts: 473
Rep Power: 20 |
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May 22, 2013, 10:53 |
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#3 |
New Member
Ano Nymous
Join Date: Oct 2011
Posts: 18
Rep Power: 15 |
Make sure that your domain is big enough. Can you post an image of the domain with the airfoil? What kind of boundary conditions did you use?
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June 11, 2013, 07:31 |
can anybody tell the meaning of this error
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#4 |
New Member
Manjunatha S
Join Date: Nov 2012
Location: Bangalore
Posts: 3
Rep Power: 14 |
ERROR #001100279 has occurred in subroutine ErrAction. |
| Message: | | Floating point exception: Overflow | | | | | | | | | | | +--------------------------------------------------------------------+ +--------------------------------------------------------------------+ | ERROR #001100279 has occurred in subroutine ErrAction. | | Message: | | Stopped in routine FPX: C_FPX_HANDLER | | | | | | | | | | | +--------------------------------------------------------------------+ |
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June 11, 2013, 07:57 |
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#5 |
Senior Member
Lance
Join Date: Mar 2009
Posts: 669
Rep Power: 22 |
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