New and existing techniques for dynamic loads analyses of flexible airplanes
Author:
Affiliation:
1. PRC—Kentron, Inc., Hampton, Virginia
2. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45309
Reference19 articles.
1. Sevart, F. D. "Development of Active Flutter Suppression Wind Tunnel Testing Technology," AFFDL-TR-74-126, Jan.1975.
2. 2Vepa, R. "On the Use of Fade Approximants to Represent Unsteady Aerodynamic Loads for Arbitrarily Small Motions of Wings," AIAA Paper 76-17, Jan.1976.
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