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Abstract
Abstract : This paper describes the application of non-asymptotic triple-deck theory of transonic shock-turbulent boundary layer interaction as a local modular element in the global calculation of supercritical airfoil flow fields. (Author)
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Abstract : This paper describes the application of non-asymptotic triple-deck theory of transonic shock-turbulent boundary layer interaction as a local modular element in the global calculation of supercritical airfoil flow fields. (Author)
Key concepts: Transonic, Boundary layer, Mechanics, Shock (circulatory), Turbulence, Aerospace engineering, Physics, Aerodynamics