Separated shock-boundary-layer interaction control using streamwise slots

Journal of Aircraft

Volumn 42, Issue 1, 2005, Pages 166-171

  Holden, H A ^a,b   Babinsky, H ^a,b  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b Department of Engineering ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; BIFURCATION (MATHEMATICS); CONTROL SYSTEMS; OPTIMIZATION; REYNOLDS NUMBER; SUPERSONIC AERODYNAMICS; WIND TUNNELS; WINGS;

DOWNSTREAM SEPARATION; MACH NUMBERS; SHOCK STRUCTURES; STREAMWISE SLOTS;

SHOCK WAVES;

EID: 13844281243     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.4687     Document Type: Article

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