Stall/Spin Flight Test Techniques with COTS Model Aircraft and Flight Data Systems
Author:
Affiliation:
1. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3225
Reference11 articles.
1. Investigations of Modifications to Improve the Spin Resistance of a High-Wing, Single-Engine, Light Airplane
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