Time-Dependent Aeroelastic Adjoint-Based Aerodynamic Shape Optimization of Helicopter Rotors in Forward Flight
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
2. University of Wyoming, Laramie, Wyoming 82071-3295
3. Parallel Geometric Algorithms, LLC, Sunnyvale, California 94087
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054962
Reference32 articles.
1. Computational fluid dynamics for aerodynamic design - Its current and future impact
2. Recent Improvements in Aerodynamic Design Optimization on Unstructured Meshes
3. Multi-Element High-Lift Configuration Design Optimization Using Viscous Continuous Adjoint Method
4. Algorithm Developments for Discrete Adjoint Methods
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