Effect of leeward flow dividers on the wing rock of a delta wing
Author:
Affiliation:
1. University of Toledo, Toledo, Ohio 43606
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46674
Reference8 articles.
1. Application of high-alpha control system concepts to a variable-sweep fighter airplane
2. 4Nguyen, L. E., Yip, L. P., and Chambers, J. R. "Self Induced Wing Rock of Slender Delta Wings,11AIAA Paper 81-1883, Aug. 1981.
3. Dynamic load measurements with delta wings undergoing self-induced roll oscillations
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