Unstructured grid solutions to a wing/pylon/store configuration using VGRID3D/USM3D
Author:
Affiliation:
1. Vigyan, Inc., Hampton, VA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-4572
Reference19 articles.
1. Transonic Euler solutions on a blunt, body-wing-canard configuration
2. Lijewski, L. E."Transonic Euler Solutions on Mutually Interfering Finned Uodies",AIAA Journal, Voluine 28, No. 6, June 1990,pp. 982-988.
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