Reliability Based Aerodynamic Shape Optimization of a Quadcopter
Author:
Affiliation:
1. BETA CAE Systems
2. Oakland University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0664
Reference26 articles.
1. Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation
2. A continuous adjoint method with objective function derivatives based on boundary integrals, for inviscid and viscous flows
3. Aerodynamic Optimization Under a Range of Operating Conditions
4. Probabilistic Approach to Free-Form Airfoil Shape Optimization Under Uncertainty
5. Robust airfoil optimization to achieve drag reduction over a range of Mach numbers
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