Variable-Fidelity Methodology for the Aerodynamic Optimization of Helicopter Rotors
Author:
Affiliation:
1. DLR, German Aerospace Center, 38108 Braunschweig, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056486
Reference32 articles.
1. Recent Applications of Design Optimization to Rotorcraft-A Survey
2. Helicopter vibration reduction using structural optimization with aeroelastic/multidisciplinary constraints - A survey
3. A Survey of Recent Developments in Rotorcraft Design Optimization
4. Numerical optimization of helicopter rotor aerodynamic performance in hover
5. Aerodynamic Shape Optimization of Hovering Rotors Using a Discrete Adjoint of the Reynolds-Averaged Navier–Stokes Equations
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