Evolutionary Algorithm Shape Optimization of a Hypersonic Flight Experiment Nose Cone
Author:
Affiliation:
1. University of New South Wales, Australian Defence Force Academy, Canberra, New South Wales 2600, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.33826
Reference30 articles.
1. Swarm Algorithm for Single- and Multiobjective Airfoil Design Optimization
2. Axisymmetric nose shapes of specified aspect ratio, optimum or close to optimum with respect to wave drag
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