Summary of Data from the Second AIAA CFD Drag Prediction Workshop (Invited)
Author:
Affiliation:
1. Cessna Aircraft Company
2. DLR Institute of Aerodynamics and Flow Technology
3. Phantom Works, The Boeing Company
4. NASA Langley Research Center
5. The Boeing Company
6. ONERA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-555
Reference41 articles.
1. Redeker, G. "DLR-F4 Wing-Body Configuration," A Selection of Experimental Test Cases for the Validation of CFD Codes, AGARD Report AR-303, Aug. 1994.
2. Hemsch, M, "Statistical Analysis of CFD Solutions from the Drag Prediction Workshop," AIAA-2002-0842.
3. Rakowitz, M., etal, "Structured and Unstructured Computations on the DLR-F4 Wing-Body Configuration," AIAA-2002-0837.
4. Mavriplis, D.J and Levy, D.W. "Transonic Drag Prediction using an Unstructured Multigrid Solver," AIAA-2002-0838.
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