Unsteady Aerodynamics of Slender Delta Wings at Large Angles of Attack
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/10.2514/3.59863
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1. Effect of a local axisymmetric imperfection on the buckling behaviorof a circular cylindrical shell under axial compression
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