Investigation of an asymmetrical shock-wave boundary-layer interaction in a supersonic planar nozzle

Canadian Aeronautics and Space Journal

Volumn 51, Issue 2, 2005, Pages 71-86

  Bourgoing, Alexis ^a   Benay, Richard ^b  

^a CNES   (France)

^b ONERA   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; MATHEMATICAL MODELS; SHOCK WAVES; SUPERSONIC AERODYNAMICS; THRUST BEARINGS; TUNNELS; TURBULENCE; BOUNDARY LAYERS; JETS; LOADS (FORCES); NOZZLES; WIND TUNNELS; NUMERICAL METHODS; REYNOLDS NUMBER; SUPERSONIC FLOW;

SHOCK INTERACTIONS; SUPERSONIC WIND TUNNEL; THRUST NOZZLES; TURBULENCE MODELS;

NOZZLES; SHOCK WAVES; BOUNDARY LAYERS;

REYNOLDS AVERAGE NAVIER-STOKES; SUPERSONIC SEPARATIONS; SUPERSONIC WIND TUNNELS; TURBULENCE MODELS; SHOCK INTERACTIONS;

EID: 27744432854     PISSN: 00082821     EISSN: None     Source Type: Journal    
DOI: 10.5589/q05-007     Document Type: Article

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