Static measurements of slender delta wing rolling moment hysteresis
Author:
Affiliation:
1. San Diego State University, San Diego, California
2. NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46024
Reference11 articles.
1. Investigation of Nonlinear Motion Experienced on a Slender-Wing Research Aircraft
2. Dynamic load measurements with delta wings undergoing self-induced roll oscillations
3. Self-induced roll oscillations measured on a delta wing/canard configuration
4. Leading edge vortex dynamics on a delta wing undergoing a wing rock motion
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