Citation: | Wu Zhigang, Yang Chao, Jing Zhiwei, et al. Dynamic response analysis of airdrop for flexible aircrafts[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(10): 1211-1217. doi: CNKI:11-2625/V.20111014.0830.002(in Chinese) |
[1] ZONA Technology Inc.ZAERO theoretical manual[M].Arizona:ZONA Technology Inc,2008 [2] 胡兆丰,肖业伦."运八"飞机投放重型货物问题的数值计算和模拟试验结果.BH-B543,1980 Hu Zhaofeng,Xiao Yelun.Numerical calculation and simulating test results of heavy cargo airdrop for Y-8 airplane.BH-B543,1980(in Chinese) [3] 傅百先.Y-8飞机连续空投纵向动态分析[J].飞行力学,1993,11(1):80-87 Fu Baixian.The longitudinal dynamic analysis of Y-8 airplane in continuous airdrop[J].Flight Dynamics,1993,11(1):80-87 (in Chinese) [4] 孙宝亭.飞机连投货物实时仿真软件及应用[J].北京航空航天大学学报,1994,20(1):71-77 Sun Baoting.A real-time simulation software of sequential airdropping of cargoes from aircraft and its application[J].Journal of Beijing University of Aeronautics and Astronautics,1994,20(1):71-77 (in Chinese) [5] Chen Jie,Shi Zhongke.Aircraft modeling and simulation with cargo moving inside[J].Chinese Journal of Aeronautics,2009,22(2):191-197 [6] 杨妙升.运输机空投的飞行动力学建模及仿真.北京:北京航空航天大学航空科学与工程学院,2010 Yang Miaosheng.Flight dynamics modeling and simulation for transport airdrop.Beijing:School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,2010 (in Chinese) [7] Zhang S J,Meganathan A,Jain K.Effects of store separation on the aeroelastic behavior of wings.AIAA 2008-6241,2008 [8] Miguel A L,Michael R W.C-17A cargo airdrop testing.AIAA 95-1578-CP,1995 [9] Marti S K,Nesrin S K,Hudson G C.Flight testing of a gravity air launch method to enable responsive space access.AIAA 2007-6146,2007 [10] 吴志刚.飞行器气动伺服弹性的建模、分析与综合研究.北京:北京航空航天大学航空科学与工程学院,2004 Wu Zhigang.Studies on aeroservoelastic modeling,analysis and synthesis of flight vehicles.Beijing:School of Aeronautic Science and Engineering,Beijing University of Aeronautics and Astronautics,2004 (in Chinese) [11] 王文亮,杜作润.结构振动与动态子结构方法[M].上海:复旦大学出版社,1985 Wang Wenliang,Du Zuorun.Structural vibration and dynamic sub-structure method[M].Shanghai:Fudan University Press,1985(in Chinese) [12] Karpel M.Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling[J].Journal of Aircraft,1982,19(3):221-227 [13] Wu Zhigang,Yang Chao.Flight loads and dynamic of flexible air vechiles[J].Chinese Journal of Aeronautics,2004,17(1):17-22
|