Reversed flow over airfoil in ANSYS -- CFD Online Discussion Forums

April 30, 2014, 11:29

Reversed flow over airfoil in ANSYS

shoaib_aero

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Shoaib

Join Date: Apr 2014

Posts: 3

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I am simulating flow over an RAE2822 airfoil with forward sweep configuration.
After applying all boundary conditions, when I run the solver, everything is normal except in post processing, the lower pressure is on the lower camber of airfoil instead of upper camber. The values seem logical and correct except that they should be on opposite cambers. I am confused about this.

Any suggestions and advice would be really appreciated.

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