Control of an oblique shock/boundary-layer interaction with aeroelastic mesoflaps

AIAA Journal

Volumn 40, Issue 12, 2002, Pages 2456-2466

  Gefroh, Derek ^a   Loth, Eric ^a   Dutton, Craig ^a   McIlwain, Stephen ^a  

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

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW VISUALIZATION; PRESSURE MEASUREMENT; REYNOLDS NUMBER; SHOCK WAVES; SUPERSONIC AERODYNAMICS; SUPERSONIC FLOW; THREE DIMENSIONAL; TURBULENCE; VELOCITY MEASUREMENT; WIND TUNNELS; WINGS;

AEROELASTIC MESOFLAPS; FLAPS; OBLIQUE SHOCK INTERACTION; PASSIVE CAVITY RECIRCULATION; SHADOWGRAPH FLOW VISUALIZATIONS; SHOCK BOUNDARY LAYER INTERACTION; STAGNATION PRESSURE PROFILES; SURFACE PRESSURE MEASUREMENTS;

AEROSPACE ENGINEERING;

EID: 0036935111     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1589     Document Type: Article

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