Microramp flow control of normal shock/boundary-layer interactions

AIAA Journal

Volumn 48, Issue 11, 2010, Pages 2529-2542

  Herges, Thomas ^a,b   Kroeker, Erik ^a,b   Elliott, Greg ^a,b   Dutton, Craig ^a,b  

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

^b Department of Aerospace Engineering ^*  (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL METHODOLOGY; DISPLACEMENT THICKNESS; ENGINE INLETS; LAYER INTERACTION; MASS FLOW; MOMENTUM THICKNESS; PARTICLE IMAGE VELOCIMETRIES; PRESSURE SENSITIVE PAINTS; PROPULSION SYSTEM EFFICIENCY; QUANTITATIVE MEASUREMENT; SCHLIEREN PHOTOGRAPHY; SHAPE FACTOR; SHOCK INTERACTIONS; SKIN FRICTION COEFFICIENT; SUB-BOUNDARY; SURFACE OIL FLOW; TURBULENT BOUNDARY LAYERS; VORTEX GENERATORS;

BOUNDARY LAYER FLOW; FLOW VISUALIZATION; FRICTION; INTAKE SYSTEMS; PAINT; PROPULSION; VELOCITY MEASUREMENT;

ATMOSPHERIC BOUNDARY LAYER;

EID: 78650402536     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050313     Document Type: Conference Paper

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