Laminar subsonic, supersonic, and transonic boundary-layer flow past a flat plate

AIAA Journal

Volumn 44, Issue 1, 2006, Pages 102-107

  Otta, S P ^a,b,c   Rothmayer, A P ^a,b,c  

^a IOWA STATE UNIVERSITY   (United States)

^b Department of Aerospace Engineering and Engineering Mechanics ^*  (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FALKNER-SKAN SOLUTIONS; FLAT PLATES; MACH NUMBER;

COMPRESSIBLE FLOW; LAMINAR FLOW; PLATES (STRUCTURAL COMPONENTS); SUBSONIC FLOW; SUPERSONIC FLOW; TRANSONIC FLOW;

BOUNDARY LAYER FLOW;

EID: 31344474349     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.16168     Document Type: Article

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