Citation: | GUO Delong, REN Yunyan, XU Yuxin, LI Yongpeng, LI Xudong, YANG Xiang. Effect of explosion location on impact response of titanium alloy directional detonation container[J]. Explosion And Shock Waves, 2024, 44(2): 025102. doi: 10.11883/bzycj-2023-0126 |
[1] |
Flight Safety Foundation. ASN Aviation safety database [EB/OL]. 2022. http://aviation-safety.net/database/year/2022/1.
|
[2] |
FAR Part 25 Amendment No: 25-127. Security considerations requirements for transport gategory airplanes [S]. United States: Federal Aviation Administration, 2008.
|
[3] |
14 CFR Parts 25 Airworthiness standards: transport category airplane [S]. Washington: Federal Aviation Administration, 2013.
|
[4] |
CCAR-121-R5 大型飞机公共航空运输承运人运行合格审定规则 [Z]. 中国民用航空局, 2017.
|
[5] |
MASI F, MARIANO P M, VANNUCCI P. Blast actions in aircrafts: an integrated methodology for designing protection devices [J]. Engineering Structures, 2018, 175: 895–911. DOI: 10.1016/j.engstruct.2018.08.082.
|
[6] |
DANG X L, CHAN P C. Design and test of a blast shield for Boeing 737 overhead compartment [J]. Shock and Vibration, 2006, 13(6): 547063. DOI: 10.1155/2006/547063.
|
[7] |
LANGDON G S, KRIEK S, NURICK G N. Influence of venting on the response of scaled aircraft luggage containers subjected to internal blast loading [J]. International Journal of Impact Engineering, 2020, 141: 103567. DOI: 10.1016/j.ijimpeng.2020.103567.
|
[8] |
Civil Aviation Authority. Aircraft hardening research programme-final overview report: CAA paper 2001/9 [R]. London: CAA, 2001.
|
[9] |
陆鹏, 郭忠宝, 杨超. 民用飞机最小风险炸弹位置适航符合性验证方法研究 [J]. 民用飞机设计与研究, 2016(4): 6–12. DOI: 10.19416/j.cnki.1674-9804.2016.04.002.
LU P, GUO Z B, YANG C. Verification method investigation of airworthiness compliance for civil aircraft least risk bomb location design [J]. Civil Aircraft Design & Research, 2016(4): 6–12. DOI: 10.19416/j.cnki.1674-9804.2016.04.002.
|
[10] |
冯振宇, 傅博宇, 解江, 等. 爆炸冲击载荷下机身壁板的动态响应 [J]. 航空学报, 2022, 43(6): 525513. DOI: 10.7527/S1000-6893.2021.25513.
FENG Z Y, FU B Y, XIE J, et al. Dynamic response of fuselage panel under explosive impact load [J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(6): 525513. DOI: 10.7527/S1000-6893.2021.25513.
|
[11] |
刘宗兴, 刘军, 李维娜. 爆炸冲击载荷下典型机身结构动响应及破坏 [J]. 航空学报, 2021, 42(2): 224252. DOI: 10.7527/S1000-6893.2020.24252.
LIU Z X, LIU J, LI W N. Dynamic response and failure of typical fuselage structure under blast impact load [J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(2): 224252. DOI: 10.7527/S1000-6893.2020.24252.
|
[12] |
朱铮铮, 冯蕴雯, 薛小峰, 等. 一种民机客舱便携式定向防爆装置: CN106197184A [P]. 2016-12-07.
|
[13] |
韩璐, 苏健军, 张玉磊, 等. 一种聚能泄压民机客舱定向防爆装置: CN109780956A [P]. 2019-05-21.
|
[14] |
李永鹏, 徐豫新, 杨祥, 等. 冲击载荷作用下机身壁板破坏效应及结构优化 [J]. 振动与冲击, 2023, 42(14): 40–47. DOI: 10.13465/j.cnki.jvs.2023.14.005.
LI Y P, XU Y X, YANG X, et al. Failure effect and structure optimization of a fuselage panel under impact load [J]. Journal of Vibration and Shock, 2023, 42(14): 40–47. DOI: 10.13465/j.cnki.jvs.2023.14.005.
|
[15] |
WANG X M, SHI J. Validation of Johnson-Cook plasticity and damage model using impact experiment [J]. International Journal of Impact Engineering, 2013, 60: 67–75. DOI: 10.1016/j.ijimpeng.2013.04.010.
|
[16] |
戴志成. 飞机断离销剪切强度有限元与实验研究 [D]. 沈阳: 沈阳理工大学, 2017.
DAI Z C. Finite element and experimental study on shear strength of aircraft fuse pin [D]. Shenyang: Shenyang Ligong University, 2017.
|
[17] |
CASTEDO R, NATALE M, LÓPEZ L M, et al. Estimation of Jones-Wilkins-Lee parameters of emulsion explosives using cylinder tests and their numerical validation [J]. International Journal of Rock Mechanics and Mining Sciences, 2018, 112: 290–301. DOI: 10.1016/j.ijrmms.2018.10.027.
|
[18] |
LEE E, FINGER M, COLLINS W. JWL equation of state coefficients for high explosives: UCID-16189 [R]. Livermore: Lawrence Livermore National Laboratory, 1973. DOI: 10.2172/4479737.
|