Simulations of Normal Shock-Wave/Boundary-Layer Interaction Control Using Mesoflaps

Journal of Propulsion and Power

Volumn 20, Issue 2, 2004, Pages 344-352

  Jaiman, R K ^a,b   Loth, E ^a,c   Dutton, J C ^a,b  

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

^b Department of Aerospace Engineering ^*

^c 306 Talbot Laboratory   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; COMPUTER SIMULATION; DRAG; FEEDBACK CONTROL; SUPERSONIC FLOW;

MESOFLAPS; STAGNATION PRESSURE; STEADY-STATE DEFLECTIONS;

SHOCK WAVES;

EID: 1842787754     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.9258     Document Type: Article

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