Aerodynamic design of supersonic cruise wings with a calibrated linearized theory
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
2. Lockheed Engineering and Sciences Company, Hampton, Virginia 23666
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46452
Reference25 articles.
1. Wing design code using three-dimensional Euler equations and optimization
2. An assessment of current methods for drag-due-to-lift minimization at supersonic speeds
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