Transonic drag prediction on a DLR-F6 transport configuration using unstructured grid solvers

AIAA Paper

Volumn , Issue , 2004, Pages 5390-5417

  Lee Rausch, E M ^a   Frink, N T ^b   Mavriplis, D J ^c   Rausch, R D ^b   Milholen, W E ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA LaRC   (United States)

^c UNIVERSITY OF WYOMING   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BOUNDARY CONDITIONS; COMPUTATIONAL FLUID DYNAMICS; FLOW VISUALIZATION; PRESSURE EFFECTS; SURFACE TESTING; TRANSONIC AERODYNAMICS; TURBULENT FLOW; VISCOUS FLOW; WIND TUNNELS;

GRID REFINEMENT; GRID SOLVERS; SURFACE PRESSURE; TRANSONIC DRAG PREDICTION;

DRAG;

EID: 2942714929     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-554     Document Type: Conference Paper

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