Evaluation of RANS Solutions for 3D Benchmark Configurations with HPCMP CREATE~(TM)-AV Kestrel

摘要

HPCMP CREATE™-AV Kestrel is used to evaluate RANS solutions for two 3D benchmark configurations provided by the NASA Langley Research Center Turbulence Modeling Resource. These include turbulent flow over a smooth body of revolution - a hemisphere-cylinder - at various angles of attack as well as turbulent flow over a transonic ONERA M6 wing at a single angle of attack. Computed solutions are compared to experimental data and to reference CFD solutions available on the Turbulence Modeling Resource.