Multi-Objective Hypersonic Entry Aeroshell Shape Optimization
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.41136
Reference14 articles.
1. Aerothermal heating predictions for Mars Microprobe
2. The rationale for an aeroassist flight experiment
3. Hypersonic and High-Temperature Gas Dynamics, Second Edition
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