In-Flight Measurement of Wing Surface Pressures on a Small-Scale UAV During Stall/Spin Maneuvers
Author:
Affiliation:
1. Stanford University
2. King Abdulaziz City for Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3652
Reference14 articles.
1. Approaches to Automatic Stall/Spin Detection Based on Small-Scale UAV Flight Testing
2. Flight Testing of a Model Aircraft with Trailing-Edge Flaps Optimized for Lift Distribution Control
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