Investigations on shock control bumps for infinite swept wings

2nd AIAA Flow Control Conference

Volumn , Issue , 2004, Pages

  Kutzbach, Martin ^a   Lutz, Thorsten ^a   Wagner, Siegfried ^a  

^a UNIVERSITY OF STUTTGART   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE WING; ANALYSIS TOOLS; ITS EFFICIENCIES; MIXING CHARACTER; NUMERICAL OPTIMIZATIONS; SHOCK CONTROL; TWO-DIMENSIONAL AIRFOILS; WAVE DRAGS;

BOUNDARY LAYERS; FLOW CONTROL; SHOCK ABSORBERS; SWEPT WINGS; TRANSPORT AIRCRAFT; TURBULENCE MODELS;

OPTIMIZATION;

EID: 84897802485     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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