Effects of Rolling Maneuver on Divergence and Flutter of Aircraft Wing Store
Author:
Affiliation:
1. Shiraz University, 71345 Shiraz, Iran
2. Clarkson University, Potsdam, New York 13699-5725
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.40463
Reference25 articles.
1. The Flutter of a Uniform Cantilever Wing
2. The Flutter of a Uniform Wing With Tip Weights
3. Transonic Flutter Analysis of a Rectangular Wing with Conventional Airfoil Sections
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