Application of Simulation Design Optimization Techniques in Aerospace Engineering

Author:

Kanazaki Masahiro1

Affiliation:

1. Tokyo Meropolitan University

Publisher

Institute of Electrical Engineers of Japan (IEE Japan)

Subject

Electrical and Electronic Engineering

Reference21 articles.

1. (1) M. Kanazaki, S. Obayashi, and K. Nakahashi : “Exhaust Manifold Design with Tapered Pipes Using Divided Range MOGA”, Engineering Optimization, Taylor and Francis, Vol. 36, No. 2, pp. 149-164 (2004)

2. (2) M. Kanazaki and S. Jeong : “High-lift Airfoil Design Using Kriging based MOGA and Data Mining”, The Korean Society for Aeronautical & Space Sciences Int J, Vol. 8, No. 2, pp. 28-36 (2007)

3. (3) M. Kanazaki, Y. Yokokawa, M. Murayama, T. Ito, S. Jeong, and K. Yamamoto : “Nacelle Chine Installation Based on Wind Tunnel Test Using Efficient Design Exploration”, T Japan Society and Space Science, Vol. 51, No. 173, pp. 146-150 (2008)

4. (4) M. Kanazaki, N. Seto, and S. Jeong : “Knowledge Discovery for Multi-Disciplinary Design of Silent Super Sonic Transport Based on Efficient Global Optimization”, Proc 6th China-Japan-Korea Joint Symposium on Optimization of Structural and Mechanical Systems, [CDROM] (2010)

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