Pneumatic concept for tip-stall control of cranked-arrow wings
Author:
Affiliation:
1. ViGYAN, Inc., Hampton, Virginia 23666
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46662
Reference9 articles.
1. 2Antani, D. L., and Morgenstern, J. M. "HSCT High-Lift Aerodynamic Technology Requirements/' AIAA Paper 92-4228, 1992.
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