Boundary layer stability calculations of the HIFiRE flight 1 vehicle in the LaRC 20-Inch Mach 6 air tunnel

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Alba, Christopher E ^a,b   Johnson, Heath B ^a   Bartkowicz, Matthew D ^a   Candler, Graham V ^a  

^a University of Minnesota   (United States)

^b USAF   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLIGHT SIMULATORS; HYPERSONIC VEHICLES; NASA; REYNOLDS NUMBER; THERMODYNAMICS;

BOUNDARY LAYER STABILITIES; BOUNDARY LAYER STABILITY ANALYSIS; CFD SIMULATIONS; DISTURBANCE GROWTH; INTERNATIONAL FLIGHTS; NASA LANGLEY RESEARCH CENTER; TRANSITION LOCATIONS;

HYPERSONIC BOUNDARY LAYERS;

EID: 78149417836     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-505     Document Type: Conference Paper

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