Drag prediction for the DLR-F6 wing-body configuration using the edge solver

Journal of Aircraft

Volumn 45, Issue 3, 2008, Pages 837-847

  Eliasson, Peter ^a,b   Peng, Shia Hui ^a,b  

^a SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^b Department of Computational Physics ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; DRAG; FLOW SEPARATION; FORECASTING; FUSELAGES; REYNOLDS NUMBER; SUBSONIC AERODYNAMICS;

GRID CONVERGENCE; NUMERICAL INVESTIGATIONS; NUMERICAL RESULTS; SEPARATION BUBBLE; SEPARATION REGIONS; UNSTRUCTURED GRID; WING TRAILING EDGE; WING-BODY CONFIGURATIONS;

WINGS;

EID: 46449119386     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.31252     Document Type: Conference Paper

References (20)

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