An implicit-explicit dirichlet-based field panel method for transonic aircraft design

20th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2002, Pages

  Gebhardt, Lutz ^a   Fokin, Dmitri ^a   Lutz, Thorsten ^a   Wagner, Siegfried ^a  

^a UNIVERSITY OF STUTTGART   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; BOUNDARY CONDITIONS; BOUNDARY ELEMENT METHOD; COMPRESSIBILITY; INTEGRODIFFERENTIAL EQUATIONS; ITERATIVE METHODS; NONLINEAR EQUATIONS; SAILING VESSELS; SHOCK WAVES; TRANSONIC AERODYNAMICS;

AERODYNAMIC DESIGNS; AIRCRAFT CONFIGURATIONS; CALCULATION RESULTS; COMPRESSIBILITY EFFECTS; DIRICHLET BOUNDARY CONDITION; FIELD-PANEL METHOD; ITERATION PROCEDURE; NON-LINEAR INTEGRO-DIFFERENTIAL EQUATIONS;

SUPERSONIC AIRCRAFT;

EID: 85067319091     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-3145     Document Type: Conference Paper

References (21)

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