Shock-wave/boundary-layer interaction control using three-dimensional bumps for transonic wings

AIAA Journal

Volumn 46, Issue 6, 2008, Pages 1442-1452

  Ogawa, H ^a,c,d   Babinsky, H ^a,d   M Patzold ^b,e   T Lutz, ^b,d,e  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b UNIVERSITY OF STUTTGART   (Germany)

^c Aerodynamics Laboratory   (United Kingdom)

^d AIAA ^*  (United Kingdom)

^e Aerodynamics Group

Author keywords

[No Author keywords available]

Indexed keywords

AEROFOIL; COMPUTATIONAL STUDIES; CONTROL EFFECTIVENESS; COUNTER-ROTATING; EXPERIMENTAL INVESTIGATIONS; IN CHANNELS; LAYER INTERACTION; LOCAL FLOWS; SHOCK STRUCTURES; THREE DIMENSIONAL (3D); THREE DIMENSIONAL BUMPS; TRANSONIC WINGS; UNIVERSITY OF CAMBRIDGE; VORTEX PAIRS; WAVE DRAGS;

BOUNDARY LAYERS; DRAG REDUCTION; FLOW INTERACTIONS; SEPARATION; THREE DIMENSIONAL; WAVES;

DRAG;

EID: 45849086102     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.32049     Document Type: Article

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