The effect of the upstream boundary-layer state on the shock interaction at a compression corner

Journal of Fluid Mechanics

Volumn 122, Issue , 1982, Pages 369-394

  Hayakawa, Kiyotaka ^a,b   Squire, L C ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b PRINCETON UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS - BOUNDARY LAYER;

SHOCK WAVES;

EID: 0020178478     PISSN: 00221120     EISSN: 14697645     Source Type: Journal    
DOI: 10.1017/S0022112082002262     Document Type: Article

References (24)

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