Effect of mach number on flow past microramps

AIAA Journal

Volumn 49, Issue 1, 2011, Pages 97-110

  Lee, S ^a   Loth, E ^a   Georgiadis, N J ^b   DeBonis, J R ^b  

^a University of Illinois at Urbana Champaign   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL STUDIES; COUNTER ROTATING; EFFECTIVE DIAMETER; HIGH-SPEED; MICRO VORTEX GENERATORS; NEAR-WALL STRUCTURES; NORMAL DISTANCE; ON FLOW; PRIMARY VORTEX; SMALL SIZE; SUPERSONIC BOUNDARY LAYER; TURBULENT BOUNDARY LAYERS; TURBULENT KINETIC ENERGY; VORTEX CORES; VORTEX GENERATORS; WEAK CORRELATION;

AERODYNAMICS; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYERS; KINETIC ENERGY; MACH NUMBER; TRANSPORT AIRCRAFT; TURBULENT FLOW; WALLS (STRUCTURAL PARTITIONS);

VORTEX FLOW;

EID: 78751507045     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050267     Document Type: Article

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