Micro-ramp flow control of normal shock/boundary layer interactions

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

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

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

Author keywords

[No Author keywords available]

Indexed keywords

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

AEROSPACE ENGINEERING; BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; FLOW CONTROL; FLOW VISUALIZATION; FRICTION; INTAKE SYSTEMS; PROPULSION; RAMP GENERATORS; VELOCITY MEASUREMENT;

ATMOSPHERIC BOUNDARY LAYER;

EID: 78549284337     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

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