Previous: NACA4412 Test Case Up: NACA4412 Test Case Next: Run the NACA4412 Case This is an automatically generated documentation by LaTeX2HTML utility. In case of any issue, please, contact us at info@cfdsupport.com. Case Description The aim of this NACA4412 test case is to test turbulence models at NACA4412 airfoil profile. A NACA4412 test case is a typical test case for testing an external aerodynamics. This test case is suitable to follow the grid convergence. This test case is suitable to follow the differences in RANS, LES and DES approaches. A free-stream flows around the simple 2D airfoil profile. The pressure coefficient distribution is tested. The test case is described in NASA pages: http://turbmodels.larc.nasa.gov/naca4412sep_val.html The test case is already preset. Figure: A sketch of NACA4412 airfoil profile. OpenFOAM Training by CFD Support, CFD SUPPORT, info@cfdsupport.com +420 212 243 883 © CFD support, s.r.o., Sokolovská 270/201, 190 00 Praha 9, Czech Republic