Carbon dioxide injection for hypervelocity boundary layer stability

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2010, Pages

  Wagnild, Ross M ^a   Candler, Graham V ^a   Leyva, Ivett A ^b   Jewell, Joseph S ^c   Hornung, Hans G ^c  

^a UNIVERSITY OF MINNESOTA   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXI-SYMMETRIC FLOWS; CARBON DIOXIDE INJECTION; CONE SURFACES; FLIGHT CONDITIONS; HYPERVELOCITIES; LAYER STABILITY; NON EQUILIBRIUM; NON-EQUILIBRIUM PROCESS; NUMERICAL SIMULATION; PARABOLIZED STABILITY EQUATIONS; POROUS WALLS; SEMI-EMPIRICAL; SHOCK TUNNEL; STABILITY ANALYSIS; STABILIZING EFFECTS; TRANSITION LOCATIONS;

AEROSPACE ENGINEERING; BOUNDARY LAYERS; CARBON DIOXIDE; CONES; FLOW SIMULATION;

AUTOMOBILE BODIES;

EID: 78649891095     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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