Aircraft dynamic response to variable wing sweep geometry
Author:
Affiliation:
1. Shanghai Jiao Tong University, Shanghai, China
2. Shanghai Aircraft Company, Shanghai, China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45580
Reference5 articles.
1. Dynamics of Variable Sweep Wing Aircraft in the Course of Changing Geometry
2. The numerical computation of aircraft response to arbitrary verticalgust distributions
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