Drag Prediction for the DLR-F6 Wing-Body Configuration Using the Edge Solver
- 1 May 2008
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 45 (3), 837-847
- https://doi.org/10.2514/1.31252
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
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- Study of CFD variation on transport configurations from the second drag-prediction workshopComputers & Fluids, 2005
- Finite Volume Discretization Aspects for Viscous Flows on Mixed Unstructured GridsAIAA Journal, 1999