Art

J-GLOBAL ID：201702226040686952   Reference number：17A0161182

Multi-objective Optimization on Aerodynamic Shape of Projectile with Twisted Empennages

ねじれ尾翼の形状は多目的最適化によって最適化した。【JST・京大機械翻訳】

Author (6)： Chen Liang (School of Mechanical Engineering, Nanjing University of Science and Technology) ,  Liu Rongzhong (School of Mechanical Engineering, Nanjing University of Science and Technology) ,  Guo Rui (School of Mechanical Engineering, Nanjing University of Science and Technology) ,  Zhao Bobo (School of Mechanical Engineering, Nanjing University of Science and Technology) ,  Liu Lei (School of Mechanical Engineering, Nanjing University of Science and Technology) ,  Yang Yongliang (School of Mechanical Engineering, Nanjing University of Science and Technology)
Material： Binggong Xuebao  (Acta Armamentarii)
Volume： 37  Issue： 7  Page： 1187-1193  Publication year： 2016 
JST Material Number： C2399A  ISSN： 1000-1093  CODEN： BIXUD9  Document type： Article
Article type： 原著論文  Country of issue： China (CHN)  Language： CHINESE (ZH)

Abstract/Point： The twisted empennage structur...

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Thesaurus term： computational fluid dynamics ,  drag ,  robustness ,  *optimization ,  drag coefficient ,  *torsion(phenomenon) ,  optimum design ,  aerodynamics(gas dynamics) ,  wind tunnel test ,  rotational frequency ,  *tail assembly
Semi thesaurus term： Pareto最適化 ,  抵抗低減 ,  多目的遺伝的アルゴリズム ,  *多目的最適化 , 【Automatic Indexing@JST】

Author keywords (6)： ordnance science and technology ,  twist empennage ,  numerical simulation ,  stepwise regression analysis ,  genetic algorithm ,  multi-objective optimization

JST classification (2)： Mathematical programmings  (KA03030M) ,  Aerodynamics of aircrafts  (QK02010T)

Terms in the title (4)： ねじれ ,  尾翼 ,  多目的最適化 ,  最適化