Support System Effects on the DLR-F6 Transport Configuration in the National Transonic Facility
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-4115
Reference21 articles.
1. 4Redeker, G. "DLR-F4 Wing Body Configuration," A Selection of Experimental Test Cases for the Validation of CFD Codes, AGARD Report AR-303, Vol.2, 1994, pp.B4-B1-21.
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