Surrogate-Based Multi-Objective Aerothermodynamic Design Optimization of Hypersonic Spiked Bodies
Author:
Affiliation:
1. University of Sheffield, Sheffield, England S1 J3D, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051018
Reference39 articles.
1. Flowfield Around Spike-Tipped Bodies for High Attack Angles at Mach 4.5
2. Numerical Heat Transfer Study over Spiked Blunt Bodies at Mach 6.8
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