Viscous interaction phenomena in hypersonic wedge flow

An experimental investigation carried out to study some aspects of shock/boundary-layer interaction in a nominally two-dimensional hypersonic wedge flow is described.

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Veröffentlicht in:AIAA journal 1995-12, Vol.33 (12), p.2293-2298
Hauptverfasser: de Luca, Luigi, Cardone, Gennaro, de la Chevalerie, Dominique Aymer, Fonteneau, Alain
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container_issue 12
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container_title AIAA journal
container_volume 33
creator de Luca, Luigi
Cardone, Gennaro
de la Chevalerie, Dominique Aymer
Fonteneau, Alain
description An experimental investigation carried out to study some aspects of shock/boundary-layer interaction in a nominally two-dimensional hypersonic wedge flow is described.
doi_str_mv 10.2514/3.12982
format Article
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ispartof AIAA journal, 1995-12, Vol.33 (12), p.2293-2298
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language eng
recordid cdi_pascalfrancis_primary_2921494
source Alma/SFX Local Collection
subjects Aerodynamics
Aircraft
Aviation
Compressible flows
shock and detonation phenomena
Exact sciences and technology
Experiments
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Physics
Shock-wave interactions and shock effects
Shock-wave interactions and shockeffects
title Viscous interaction phenomena in hypersonic wedge flow
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