Boundary layer stability analysis to support the HIFiRE transition experiment

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 6, Issue , 2007, Pages 3804-3816

  Johnson, Heath B ^a,c   Alba, Chris R ^a,c   Candler, Graham V ^a,c   MacLean, Matthew ^b,c   Wadhams, Timothy ^b,c   Holden, Michael ^b,c  

^a University of Minnesota   (United States)

^b CUBRC   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; CORRELATION METHODS; FLIGHT DYNAMICS; HYPERSONIC FLOW; STABILITY;

HYPERSONIC INTERNATIONAL FLIGHT RESEARCH EXPERIMENTATION (HIFIRE); PSE METHOD; SHOCK TUNNEL; STABILITY ANALYSIS;

BOUNDARY LAYERS;

EID: 34250883944     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-311     Document Type: Conference Paper

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