Boundary layer calculations for preliminary design of wings in supersonic flow

17th Applied Aerodynamics Conference

Volumn , Issue , 1999, Pages 47-57

  Sturdza, Peter ^a   Manning, Valerie M ^a   Kroot, Ilan M ^a   Tracy, Richard R ^b  

^a 496 Lomita Mall   (United States)

^b Reno Aeronautical Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FINITE DIFFERENCE METHOD; LAMINAR FLOW; NAVIER STOKES EQUATIONS; SHAPE OPTIMIZATION; SUPERSONIC AIRCRAFT; SWEPT WINGS;

ANALYTIC SOLUTION; FAST CALCULATIONS; FINITE-DIFFERENCE ANALYSIS; FLIGHT CONDITIONS; MULTI-DISCIPLINARY OPTIMIZATIONS; NATURAL LAMINAR FLOWS; PRELIMINARY DESIGN; THREE-DIMENSIONAL BOUNDARY LAYERS;

BOUNDARY LAYERS;

EID: 84964284830     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-3104     Document Type: Conference Paper

References (18)

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