| Presentation | 1999/5/28 Design Optimization of the Next Generation SST Using Genetic Algorithms Shigeru Obayashi, Naoki Hirose, |
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| PDF Download Page | PDF download Page Link |
| Abstract(in Japanese) | (See Japanese page) |
| Abstract(in English) | This paper describes the design optimization of a wing for supersonic transport (SST) using Multi-Objective Genetic Algorithm (MOGA). The objective functions are to minimize the drag for transonic cruise, the drag for supersonic cruise and the bending moment at the wing root for supersonic cruise. The wing shape is defined by planform and warp shapes in total of 66 design variables. An Euler code is used to evaluate supersonic performance, and a potential code is used to evaluate transonic performance. To reduce the enormous total calculation time, the CFD ca1culations are parallelized on NEC SX-4 (32PE) at Computer Center of Tohoku University. The Pareto optimal solutions are obtained in the three dimensional objective function space by the present approach. One of the Pareto solutions is found to outperform an existing design based on the linearied theory. |
| Keyword(in Japanese) | (See Japanese page) |
| Keyword(in English) | Wings and Airfoil Sections / Aerodynamic Optimization / Evolutionary Computation |
| Paper # | AI99-18 |
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| Conference Information | |
| Committee | AI |
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| Conference Date | 1999/5/28(1days) |
| Place (in Japanese) | (See Japanese page) |
| Place (in English) | |
| Topics (in Japanese) | (See Japanese page) |
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| Paper Information | |
| Registration To | Artificial Intelligence and Knowledge-Based Processing (AI) |
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| Language | JPN |
| Title (in Japanese) | (See Japanese page) |
| Sub Title (in Japanese) | (See Japanese page) |
| Title (in English) | Design Optimization of the Next Generation SST Using Genetic Algorithms |
| Sub Title (in English) | |
| Keyword(1) | Wings and Airfoil Sections |
| Keyword(2) | Aerodynamic Optimization |
| Keyword(3) | Evolutionary Computation |
| 1st Author's Name | Shigeru Obayashi |
| 1st Author's Affiliation | Department of Aeronautics and Space Engineering, Tohoku University() |
| 2nd Author's Name | Naoki Hirose |
| 2nd Author's Affiliation | Computational Science Division, National Aerospace Laboratory |
| Date | 1999/5/28 |
| Paper # | AI99-18 |
| Volume (vol) | vol.99 |
| Number (no) | 96 |
| Page | pp.pp.- |
| #Pages | 7 |
| Date of Issue | |