Aerodynamic Shape Optimization of an Adaptive Morphing Trailing-Edge Wing
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033116
Reference31 articles.
1. Design and application of compliant mechanisms for morphing aircraft structures
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4. Aeroservoelastic Design Optimization of a Flexible Wing
5. Automatic Differentiation Adjoint of the Reynolds-Averaged Navier-Stokes Equations with a Turbulence Model
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