Momentum Vector Control for Spin Recovery
Author:
Affiliation:
1. Systems Technology, Inc., Hawthorne, California 90250-7083
2. Wichita State University, Wichita, Kansas 67260-0044
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.4334
Reference22 articles.
1. Numerical lifting line theory applied to drooped leading-edge wings below and above stall
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