Art

J-GLOBAL ID：201702239928607334   Reference number：17A0161130

Research on Aerodynamic Characteristics of Terminal Sensitive Projectile with S-C Shaped Elastic Wings

弾性翼列の空力特性を研究した。【JST・京大機械翻訳】

Author (4)： Lyu Shengtao (School of Chemistry Engineering, Nanjing University of Science and Technology) ,  Liu Rongzhong (Ministerial Key Laboratory of ZNDY, Nanjing University of Science and Technology) ,  Guo Rui (Ministerial Key Laboratory of ZNDY, Nanjing University of Science and Technology) ,  Ma Xiaodong (Ministerial Key Laboratory of ZNDY, Nanjing University of Science and Technology)
Material： Binggong Xuebao  (Acta Armamentarii)
Volume： 37  Issue： 5  Page： 785-790  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： Two-way fluid-structure intera...

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Thesaurus term： rigidity ,  aerodynamics(gas dynamics) ,  torque ,  *aerodynamic characteristic ,  simulation ,  tail assembly ,  lift coefficient ,  two dimensional flow ,  angle of attack ,  *elasticity(mechanical property) ,  aeroelasticity ,  drag coefficient ,  *cascade
Semi thesaurus term： 自由飛行 , 【Automatic Indexing@JST】

Author keywords (5)： ordnance science and technology ,  non-parachute terminal sensitive projectile ,  aeroelasticity ,  aerodynamic characteristics ,  free flight test

JST classification (1)： Aerodynamics of aircrafts  (QK02010T)

Terms in the title (4)： 弾性 ,  翼列 ,  空力特性 ,  研究