Measurements of the triple shock wave/turbulent boundary-layer interaction

A joint experimental and computational study that examined the flowfield structure created by three crossing oblique shock waves interacting with a turbulent boundary layer is described.

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Bibliographic Details
Published in:AIAA journal 1996-01, Vol.34 (1), p.57-64
Main Authors: Garrison, T. J, Settles, G. S, Horstman, C. C
Format: Article
Language:English
Subjects:
Aircraft
Boundary layer and shear turbulence
Boundary layers
Compressible flows
shock and detonation phenomena
Computational complexity
Computational fluid dynamics
Exact sciences and technology
Flow measurement
Flow visualization
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Mathematical models
Physics
Shock waves
Shock-wave interactions and shock effects
Shock-wave interactions and shockeffects
Turbulence
Turbulent flow
Turbulent flows, convection, and heat transfer
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Description
Summary:A joint experimental and computational study that examined the flowfield structure created by three crossing oblique shock waves interacting with a turbulent boundary layer is described.
ISSN:0001-1452
1533-385X
DOI:10.2514/3.12864