Normal shock/boundary-layer interaction control using aeroelastic mesoflaps

Journal of Propulsion and Power

Volumn 19, Issue 3, 2003, Pages 464-472

  Hafenrichter, Everett S ^a   Lee, Yeol ^a,b   Dutton, J Craig ^a   Loth, Eric ^a  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^b Hankuk Aviation University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT PARTS AND EQUIPMENT; BOUNDARY LAYERS; FLOW VISUALIZATION; PRESSURE DISTRIBUTION; SHOCK WAVES; WIND TUNNELS;

AEROELASTIC MESOFLAPS; AEROELASTIC RECIRCULATING TRANSPIRATION; FLAPS; FLOW CONTROL SYSTEM; NORMAL SHOCK BOUNDARY LAYER INTERACTION CONTROL;

SUPERSONIC AIRCRAFT;

EID: 0037505129     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.6130     Document Type: Article

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