Accession Number : ADA017362
Title : Analytical Theory of Transonic Normal Shock-Boundary Layer Interaction.
Corporate Author : VIRGINIA POLYTECHNIC INST AND STATE UNIV BLACKSBURG COLL OF ENGINEERING
Report Date : SEP 1975
Pagination or Media Count : 10
Abstract : This paper describes an approximate analytical theory of the nonseparating transonic interaction of a weak normal shock with an isobaric laminar or turbulent boundary layer. The resulting mixed rotation transonic flow boundary value problem is solved analytically by Fourier transformation methods. Numerical results are presented for turbulent boundary layer pressure distributions, flow geometry and skin friction.
Descriptors : *Boundary layer flow, *Shock waves, *Transonic characteristics, Laminar boundary layer, Turbulent boundary layer, Interactions, Numerical methods and procedures, Rotation, Shear properties, Mathematical models, Pressure distribution, Skin friction, Fourier transformation
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE