Physics and modeling of unsteady shock wave/boundary layer interactions over transonic airfoils by numerical simulation
Shock wave/boundary layer interactions arising in the transonic flow over airfoils are studied numerically using different levels of turbulence modeling. The simulations employ standard URANS models suitable for aerodynamics and hybrid RANS-LES methods. The use of a compressibility correction for on...
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| Format: | Others |
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2014
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| Online Access: | http://oatao.univ-toulouse.fr/11817/1/grossi.pdf |