Physics and modeling of unsteady shock wave/boundary layer interactions over transonic airfoils by numerical simulation

Physics and modeling of unsteady shock wave/boundary layer interactions over transonic airfoils by numerical simulation

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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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Bibliographic Details
Main Author:	Grossi, Fernando
Format:	Others
Published:	2014
Online Access:	http://oatao.univ-toulouse.fr/11817/1/grossi.pdf

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