Approximate Nonlinear Slender Wing Aerodynamics
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Inc., Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58915
Reference26 articles.
1. Analysis of flow separation effects on the dynamics of a large space booster
2. Progress on the launch-vehicle buffeting problem
3. Unsteady Aerodynamics of Slender Delta Wings at Large Angles of Attack
4. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
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