Comparison of Point Design and Range-Based Objectives for Transonic Aerofoil Optimization
Author:
Affiliation:
1. University of Bristol, Bristol, England BS8 1TR, United Kingdom
Funder
Engineering and Physical Sciences Research Council
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056627
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