Multipoint Nose Shape Optimization of Space Launcher Using Response Surface Method
Author:
Affiliation:
1. Konkuk University, Seoul 143-701, Republic of Korea
2. Agency for Defense Development, Daejeon 305-605, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.11228
Reference26 articles.
1. Two-point transonic airfoil design using optimization for improved off-design performance
2. Dual-Point Design of Transonic Airfoils Using the Hybrid Inverse Optimization Method
3. Optimal design of a space launch vehicle using response surface method
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