[1] |
肖华军.航空供氧防护装备生理学[M].北京:军事医学科学出版社, 2008:107-110 Xiao Huajun. Aviation oxygen protection equipment physiology[M].Beijing:Military Medicine Science Press, 2008:107-110 (in Chinese)
|
[2] |
Murugan S, Flores E S. Optimal design of variable fiber spacing composites for aircraft skins[J].Composite Structures, 2012, 94(4) :626-633
|
[3] |
张彦考.全复合材料舱段组合结构优化设计[J].西北工业大学学报, 2008, 51(11):1048-1050 Zhang Yankao.Composite structural optimization design of all composite material cabin[J].Journal of Northwestern Polytechnical University, 2008, 51(11):1048-1050(in Chinese)
|
[4] |
Simmons M C, Schleyer G K.Pressure loading of aircraft structural panels[J].Thin-Walled Structures, 2009, 47(4):496-506
|
[5] |
Lewis S J.The use of carbon fibre composites on military aircraft[J].Composites Manufacturing, 2006, 17(1):95-103
|
[6] |
Kotzakolios T, Vlachos D E, Kostopoulos V.Response of metal composite laminate fuselage structures using finite element modelling[J].Composite Structures, 2011, 93(5):665-681
|
[7] |
刘丰睿, 赵丽滨, 刘海涛.复合材料舱段三维应力分析及设计[J].材料工程, 2008, 52(5):449-450 Liu Fengrui, Zhao Libin, Liu Haitao.Analysis and design of composite material cabin three-dimension stress[J].Materials Engineering, 2008, 52(5):449-450(in Chinese)
|
[8] |
冯军.复合材料技术在当代飞机结构上的应用[J].航空制造技术, 2009, 17(2):101-102 Feng Jun.The application of composite material technology in modern aircraft structure[J].Aviation Manufacturing Technology, 2009, 17(2):101-102(in Chinese)
|
[9] |
Ardema M D, Chambers M C, Patron A P.The weight estimation and analysis of fuselage and wing of transport aircraft[J].Technical Memorandum, 2009, 32(5):445-450
|
[10] |
Heimbs S, Vogt D, Hartnack R.Numerical simulation of aircraft interior components under loads[J].Int J Crash Worthiness, 2008, 23(5):511-521
|
[11] |
Langdon G S, Nurick G N, Cantwell W J.The response of fibre metal laminates panels subjected to uniformly distributed loading[J].Eur J Mech A/Solids, 2009, 32(2):107-115
|