Direct numerical simulations of instability-wave generation and propagation in supersonic boundary layers

Lecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)

Volumn 2668, Issue , 2003, Pages 859-870

  Jiang, Li ^a   Choudhari, Meelan ^b   Chang, Chau Lyan ^b   Liu, Chaoqun ^a  

^a UNIVERSITY OF TEXAS AT ARLINGTON   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; DIRECT NUMERICAL SIMULATION; NUMERICAL MODELS; SUPERSONIC AIRCRAFT; SWEPT WINGS;

BOUNDARY LAYER TRANSITIONS; COMPONENT PERFORMANCE; CROSS-FLOW INSTABILITIES; ENVIRONMENTAL CHALLENGES; PARABOLIZED STABILITY EQUATIONS; STRINGENT REQUIREMENT; SUPERSONIC BOUNDARY LAYER; SWEPT-WING BOUNDARY LAYERS;

FIGHTER AIRCRAFT;

EID: 30744431585     PISSN: 03029743     EISSN: 16113349     Source Type: Book Series    
DOI: 10.1007/3-540-44843-8_93     Document Type: Article

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