Weight Indexing for Wing-Shape Multi-Objective Optimization
Author:
Affiliation:
1. Flight Performance and Propulsion Group, Faculty of Aerospace Engineering, Delft University of Technology, 2629 HS Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052406
Reference44 articles.
1. HicksR. M.MurmanE. M.VanderplaatsG. N. “An Assessment of Airfoil Design by Numerical Optimization,” NASA TM-X-3092, July 1974.
2. Wing Design by Numerical Optimization
3. BarnesJ. “Math Modeling of Airfoil Geometry,” SAE TP-961317, Warrendale, PA, 1996.
4. Universal Parametric Geometry Representation Method
5. Extension to the Class-Shape-Transformation Method Based on B-Splines
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