Impact of airfoil profile on the supersonic aerodynamics of delta wings
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45364
Reference9 articles.
1. SC3 - A wing concept for supersonic maneuvering
2. 3Siclari, M.J.'The NCOREL Computer Program for 3D Nonlinear Supersonic Potential Flow Computations," NASA CR-3694, Aug. 1983.
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