Transonic Drag Prediction on a DLR-F6 Transport Configuration Using Unstructured Grid Solvers
Author:
Affiliation:
1. NASA Langley
2. National Institute of Aerospace
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-554
Reference23 articles.
1. 1Levy,D.W.,Zickuhr,T.,Vassberg,J.,Agrawal,S.,Wahls,R.A., Pirzaheh, S., and Hemsch, M. J. "Summary of Data from the First AIAACFDDragPredictionWorkshop,"Tech.Rep.AIAA-2002-0841, Jan.2002.
2. 3Rakowitz, M., Sutcliffe, M., Eisfeld, B., Schwamborn, D. Bleecke, H., and Fassbender, J. "Structured and Unstructured Computations on the DLR-F4 Wing-Body Configuration," Tech. Rep. AIAA-2002-0837, Jan. 2002.
3. 4Mavriplis,D.J.andLevy,D.W."TransonicDragPredictionUsing an Unstructured Multigrid Solver," Tech. Rep. AIAA-2002-0838, Jan. 2002.
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