NO PLIF study of hypersonic transition over a discrete hemispherical roughness element

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

Volumn , Issue , 2009, Pages

  Danehy, Paul M ^a   Bathel, Brett ^a,b   Ivey, Christopher ^a,c   Inman, Jennifer A ^a   Jones, Stephen B ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b UNIVERSITY OF VIRGINIA   (United States)

^c JOHNS HOPKINS UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; HYPERSONIC FLOW; NITRIC OXIDE; REYNOLDS NUMBER; VORTEX FLOW;

ANGLES OF ATTACK; BOUNDARY LAYER THICKNESS; CFD COMPUTATION; FLAT PLATE; PLANAR LASER INDUCED FLUORESCENCE; ROUGHNESS ELEMENTS; STREAMWISE DIRECTIONS; TURBULENT STRUCTURES;

ANGLE OF ATTACK;

EID: 78549245132     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-394     Document Type: Conference Paper

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