Some observations on the mechanism of aircraft wing rock
Author:
Affiliation:
1. Northrop Corp., Aircraft Div., Hawthorne, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1978-1456
Reference5 articles.
1. Northrop F-5A aircraft transonic buffet pressure data acquisition and response analysis
2. Unsteady aerodynamic and stall effects on helicopter rotor blade airfoil sections.
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