Flow model for predicting normal shock wave induced vortex breakdown

AIAA Journal

Volumn 35, Issue 10, 1997, Pages 1589-1596

  Smart, M K ^a,c   Kalkhoran, I M ^b,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b POLYTECHNIC UNIVERSITY   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSIBILITY OF LIQUIDS; MATHEMATICAL MODELS; SHOCK WAVES; SUPERSONIC FLOW; VELOCITY;

COMPRESSIBILITY EFFECTS; FLOW MODEL; MACH NUMBER; SHOCK WAVE VORTEX INTERACTION; SWIRL; VORTEX BREAKDOWN;

VORTEX FLOW;

EID: 0031259435     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.17     Document Type: Article

References (17)

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