Evaluation of Quasi-Static Gust Loads Certification Methods for High-Altitude Long-Endurance Aircraft
Author:
Affiliation:
1. Department of Aerospace and Ocean Engineering, Virginia Polytechnical Institute and State University, Blacksburg, Virginia 24061
2. AFRL/MSTC, U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031872
Reference32 articles.
1. LuciaD. J. “The Sensorcraft Configurations: A Nonlinear Aeroservoelastic Challenge for Aviation,” AIAA Paper 2005-1943, April 2005.
2. Flight Dynamics of Highly Flexible Flying Wings
3. FloreanoD.ZuffereyJ. C.SrinivasanM. V., Flying Insects and Robots, Springer–Verlag, New York, 2009, pp. 185–205.
4. PrattK. G.WalkerW. G. “A Revised Gust-Load Formula and a Reevaluation of V-G Data Taken on Civil Transport Airplanes from 1933 to 1950,” NACA Rept. 1206, 1954.
5. HunsakerJ. C.WilsonE. D. “Report on Behavior of Aeroplanes in Gusts,” NACA Rept. 1, 1915.
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