Navier-Stokes computations on flexible advanced transport wings in transonic regime
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035-1000
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46984
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1. COMPARISON OF SUPERCRITICAL AND CONVENTIONAL WING FLUTTER CHARACTERISTICS
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4. Ensaero—A multidisciplinary program for fluid/structural interaction studies of aerospace vehicles
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