Numerical investigations on the VFE-2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Schütte, Andreas ^a   Lüdeke, Heinrich ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

DELTA WINGS; EXPERIMENTAL DATA; FLOW TOPOLOGY; HYBRID MESHES; LEADING EDGE; NUMERICAL INVESTIGATIONS; NUMERICAL RESEARCH; NUMERICAL RESULTS; NUMERICAL SIMULATION; RANS EQUATION; REYNOLDS NUMBER EFFECT; WORKING GROUPS;

AEROSPACE ENGINEERING; COMPUTER SIMULATION; REYNOLDS NUMBER; TURBULENCE MODELS;

DELTA WING AIRCRAFT;

EID: 78149463419     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

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