A New Design Method for Market-Oriented Aircraft
A New Design Method for Market-Oriented Aircraft
批准号:
11650939
负责人:
OBAYASHI Shiogeru
金额:
$2.37万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
1999
资助国家:
日本
项目状态:
已结题
起止时间:
1999 至 2001
中文摘要
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英文摘要
Toward aircraft built domestically or developed by Asian Airbus-like consortium, researches have bee conducted for market, Computational Fluid Dynamics (CFD), and design optimization. Market study focused on feasibility of supersonic regional transport, which connects Asian cities within one-day round trip. A conceptual design of supersonic regional jet has been presented. Sophisticated Evolutionary Multiobjective Optimization (EMO) has been developed and applied to supersonic wing design. This research is one of the most realistic EMO applications and has been recognized internationally.EMO searches many compromised solutions (Pareto solutions) between multiple objective functions simultaneously. The resulting set of solutions reveals design tradeoffs between conflicting design objectives. This method has been applied to supersonic wing design with four design objective and various design tradeoffs have been examined. The tradeoff study is trivial between two objectives : however, it … More will become more difficult as the number of design objectives increases. Therefore, aiming for real-world applications of EMO, visualization of Pareto solutions are studied as post-processing together with the improvement and application of EMO itself. Self-Organizing Map (SOM) has been utilized as a visualization technique of high dimensional space. Datamining of design tradeoffs between multiple design objectives are performed by using SOM of Pareto solutions in the objective function space. SOM is also confirmed to be useful as the datamining tool by mapping the solutions in design variable space because the resulting SOM represents the aerodynamic knowledge in wing design througjh the clusters of design variables.In addition to these works, researches have been performed for unstructured adjoint approach as an alternative optimization method and for extension of CFD code to fluid-structure interaction toward multidisciplinary design optimization. These activities have been reported at international conferences. Less
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大林 茂: "CFD利用の新段階-数値最適化"日本機械学会誌. 105・999. 2-7 (2001)
Shigeru Obayashi:“CFD 应用的新阶段 - 数值优化”日本机械工程学会杂志 105・999(2001 年)。
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H. - J. Kim: "Flap-Deflection Optimization for Transonic Cruise Performance Improvement of Supersonic Transport Wing"Journal of Aircraft. 38・4. 709-717 (2001)
H. - J. Kim:“超音速运输机翼的跨音速巡航性能改进的襟翼偏转优化”,《飞机杂志》38・4(2001 年)。
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Shigeru Obayashi: "Multiobjective Evolutionary Computation for Supersonic Wing-Shape Optimization"IEEE Transactions on Evolutionary Computation. 4・2. 182-187 (2000)
Shigeru Obayashi:“超音速翼形优化的多目标进化计算”IEEE 进化计算汇刊 4・2(2000 年)。
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Akira Oyama,Shigeru Obayashi,and Kazuhiro Nakahashi: "Real-Coded Adaptive Range Genetic Algorithm and Its Application to Aerodynamic Design"JSME International Journal. 43・A. 124-129 (2000)
Akira Oyama、Shigeru Obayashi 和 Kazuhiro Nakahashi:“实数编码自适应范围遗传算法及其在空气动力学设计中的应用”JSME 国际期刊 43・A。
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佐々木大輔.竹口幸宏.大林茂 中橋和博 広瀬直喜: "次世代超音速輸送機主翼の超音速と遷音速巡航の多目的最適化"日本航空宇宙学会誌. 47・551. 464-469 (1999)
佐佐木大辅、竹口幸宏、大林茂、中桥一宏、广濑直树:“用于超音速和跨音速巡航的下一代超音速运输机主翼的多目标优化”日本航空学会学报47・。 551.464-469(1999)
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