Numerical Simulation of Shock-Wave Interaction with a Laminar Boundary Layer in a Hypersonic Flow around Models with a Kink in the Generatrix

A series of experimental data obtained at the Calspan–University at Buffalo Research Center (CUBRC) and accompanying numerical calculations performed by members of the computer code testing working group were used to validate the author’s PERAT-2D computer code. The problems of a hypersonic flow of...

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Bibliographic Details
Published in:Fluid dynamics 2022-12, Vol.57 (Suppl 1), p.S97-S116
Main Author: Surzhikov, S. T.
Format: Article
Language:English
Subjects:
Analysis
Classical and Continuum Physics
Classical Mechanics
Engineering Fluid Dynamics
Fluid- and Aerodynamics
Hypersonic flow
Laminar boundary layer
Mathematical models
Numerical analysis
Physics
Physics and Astronomy
Research facilities
Shock wave interaction
Simulation methods
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Summary:A series of experimental data obtained at the Calspan–University at Buffalo Research Center (CUBRC) and accompanying numerical calculations performed by members of the computer code testing working group were used to validate the author’s PERAT-2D computer code. The problems of a hypersonic flow of molecular nitrogen around a sharp and blunt cone with a kink in the generatrix, as well as around a hollow cylinder with a sharp edge and an expanding skirt, are considered.
ISSN:0015-4628
1573-8507
DOI:10.1134/S001546282260122X