Supersonic Forward-Swept Wing Design Using Multifidelity Efficient Global Optimization
Author:
Affiliation:
1. Tokyo Metropolitan University, Tokyo 191-0065, Japan
2. Japan Aerospace Exploration Agency, Tokyo 181-0015, Japan
Funder
Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036422
Reference45 articles.
1. Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints
2. Conceptual Design of Swept-Wing Root Airfoils
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