Computational study of static and dynamic vortical flow over the delta wing SACCON configuration using the FOI flow solver Edge

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Tormalm, Magnus ^a,c   Schmidt, Stefan ^b,d  

^a SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^b DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

^c Department of Aeronautics and Systems Integration ^*  (Sweden)

^d Air Vehicles Division   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW SIMULATION; TURBULENCE MODELS;

COMPUTATIONAL STUDIES; DISCRETIZATIONS; DYNAMIC DATA; EXPERIMENTAL INVESTIGATIONS; H-REFINEMENT; MESH RESOLUTION; NUMERICAL INVESTIGATIONS; VORTICAL FLOWS;

DELTA WING AIRCRAFT;

EID: 78649501751     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4561     Document Type: Conference Paper

References (19)

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