Simulation of crossflow instability on a supersonic highly swept wing

Computers and Fluids

Volumn 29, Issue 1, 2000, Pages 33-62

  Pruett, C David ^a   Chang, Chau Lyan ^b   Streett, Craig L ^c  

^a JAMES MADISON UNIVERSITY   (United States)

^b High Technology Corporation   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

Compressible flow; Direct numerical simulation; High speed civil transport; Parabolized stability equation methodology; Stationary crossflow instability; Swept wing

Indexed keywords

EID: 0345044940     PISSN: 00457930     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7930(98)00056-5     Document Type: Article

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