Validation procedure for the analysis of shock-wave/boundary-layer interaction problems

The validation of hypersonic flow simulation in the presence of strong shock-wave/boundary-layer interaction phenomena is discussed. The equations solved are the Reynolds-averaged Navier-Stokes equations with an algebraic turbulence model.

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Bibliographic Details
Published in:AIAA journal 1994-09, Vol.32 (9), p.1820-1827
Main Authors: Grasso, F, Leone, G, Delery, J. M
Format: Article
Language:English
Subjects:
Aerodynamics
Compressible flows
shock and detonation phenomena
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Laminar boundary layers
Laminar flows
Physics
Shock-wave interactions and shock effects
Shock-wave interactions and shockeffects
Simulation
Transition to turbulence
Turbulence simulation and modeling
Turbulent flows, convection, and heat transfer
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Description
Summary:The validation of hypersonic flow simulation in the presence of strong shock-wave/boundary-layer interaction phenomena is discussed. The equations solved are the Reynolds-averaged Navier-Stokes equations with an algebraic turbulence model.
ISSN:0001-1452
1533-385X
DOI:10.2514/3.12179