[Download free pdf] Robust Aerodynamic Design of Mars Exploratory Airplane Wing: With a New Optimization Method
·•●- Koji Shimoyama ·•●-
| 2010-11-15 | Original language:English | PDF # 1 | 8.66 x.47 x5.91l,.69 | File Name: 3843371938 | 208 pages
||About the Author|He received the Ph.D. degree in aeronautics and astronautics from the University of Tokyo, Japan, in 2006. He is currently an Assistant Professor in the Institute of Fluid Science, Tohoku University, Japan. His main research interest is the r
A new robust design optimization approach "design for multi-objective six sigma (DFMOSS)" has been developed, and aerodynamic design optimizations of Mars exploratory airplane wing considering the effects of wind variations were carried out by using the DFMOSS coupled with the computational fluid dynamics (CFD) simulation. The present optimizations successfully revealed detailed trade-off information between the optimality and the robustness of aerodynamic perform...
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