Numerical solution to the glancing sidewall oblique shock wave/turbulent boundary layer interaction in three-dimensionA supersonic three-dimensional viscous forward-marching computer design code called PEPSIS is used to obtain a numerical solution of the three-dimensional problem of the interaction of a glancing sidewall oblique shock wave and a turbulent boundary layer. Very good results are obtained for a test case that was run to investigate the use of the wall-function boundary-condition approximation for a highly complex three-dimensional shock-boundary layer interaction. Two additional test cases (coarse mesh and medium mesh) are run to examine the question of near-wall resolution when no-slip boundary conditions are applied. A comparison with experimental data shows that the PEPSIS code gives excellent results in general and is practical for three-dimensional supersonic inlet calculations.
Document ID
19830035605
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, B. H. (NASA Lewis Research Center Cleveland, OH, United States)
Benson, T. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 83-0136
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting