Previous: Notes on Convergence Up: NACA4412 Test Case Next: Pressure Coefficient around the This is an automatically generated documentation by LaTeX2HTML utility. In case of any issue, please, contact us at info@cfdsupport.com. NACA4412 Simulation Results Description Subsections Pressure Coefficient around the 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