Rakowitz, M. and Sutcliffe, M. and Eisfeld, B. and Schwamborn, D. and Bleecke, H. and Faßbender, J. (2002) Structured and Unstructured Computations on the DLR-F4 Wing-Body Configuration. 40th AIAA Aerospace Science & Exhibit, 2002-01-14 - 2002-01-17, Reno (USA).
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The accuracy of the DLR structured and unstructured computational fluid dynamic (CFD) codes in predicting aircraft forces and moments on a wing-body configuration at transonic speeds is investigated. The computations form the contribution of the DLR and Airbus Deutschland to the AIAA CFD Drag Prediction Workshop in June 2001. Using a combination of a high quality grid, low levels of artificial dissipation and an advanced turbulence model, the structured code (FLOWer) was able to both qualitatively and quantitativele predict the experimentally measured drag, lift and pitching moments. In its current implementation the unstructured code (TAU) was found to be less accurate in predicting forces and moments, although qualitatively the results were good.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=2004, monograph_id=AIAA paper 2002-0837,|
|Title:||Structured and Unstructured Computations on the DLR-F4 Wing-Body Configuration|
|Keywords:||Drag Prediction Workshop, MEGAFLOW, CFD, F4|
|Event Title:||40th AIAA Aerospace Science & Exhibit|
|Event Location:||Reno (USA)|
|Event Type:||international Conference|
|Event Dates:||2002-01-14 - 2002-01-17|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Concepts & Integration|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||Claudia Grant|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 19:28|
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