Multipoint Aerodynamic High Fidelity Shape Optimization of an Isolated Engine Nacelle
Author:
Affiliation:
1. ONERA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0903
Reference14 articles.
1. Surrogate-Based Aerodynamic Shape Optimization of a Civil Aircraft Engine Nacelle
2. Aerodynamic Optimization of an Over-the-Wing-Nacelle-Mount Configuration
3. Constrained optimization of nacelle shapes in Euler flow using semianalytical sensitivity analysis
4. Iterative three-dimensional transonic wing design using integral equations
5. An inverse design method for designing isolated and wing-mounted engine nacelles
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