Numerical and experimental analyses of the vortical flow around the SACCON configuration

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Schütte, Andreas ^a   Hummel, Dietrich ^b,d   Hitzel, Stephan M ^c  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

^c AIRBUS GROUP INNOVATIONS   (Germany)

^d EADS Deutschland GmbH ^*  (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; FLIGHT ENVELOPES; FLIGHT SIMULATORS; FLOW SEPARATION; SWEPT WINGS; TURBULENCE MODELS;

ANGLES OF ATTACK; COMPLEX FLOW STRUCTURES; COMPUTATIONAL GRIDS; ENTIRE FLIGHT ENVELOPE; NUMERICAL AND EXPERIMENTAL ANALYSIS; NUMERICAL RESULTS; STABILITY AND CONTROL; VORTEX SYSTEMS;

FLIGHT CONTROL SYSTEMS;

EID: 78649527907     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4690     Document Type: Conference Paper

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