[1] Structural Assessment of Solid Propellant Grains[R].AGARD-AR-350,1997.
[2] 程靳,赵树山.断裂力学[M].北京:科学出版社,2006.
[3] Liu C T,Smith C W.Temperature and Rate Effects on Stable Crack Growth in a Particulate Composite Material[J].Experimental Mechanics,1996,36 (3): 290-295.
[4] Bencher C D,Dauskardt R H,Ritchie R O.Microstructural Damage and Fracture Processes in a Composite Solid Rocket Propellant[J].Journal of Spacecraft and Rockets,1995,32 (2): 328-334.
[5] Giuseppe S T,Victor E S,Robert T,et al.Fracture Mechanics of Composite Solid Rocket Propellant Grains: Material Testing[J].Journal of Propulsion and Power,2009,25 (1): 60-73.
[6] 屈文忠.国产HTPB复合推进剂裂纹扩展特性的实验研究[J].推进技术,1994,15(6):88-92.(QU Wen-zhong.Experimental Research on Crack Growth Behavior in HTPB Composite Propellant[J].Journal of Propulsion Technology,1994,15(6): 88-92.)
[7] 张亚,强洪夫,杨月诚.国产HTPB复合固体推进剂I-II型裂纹断裂性能实验研究[J].含能材料,2007,15 (4): 359-362.
[8] 周广盼,尹晓春,鞠玉涛,等.HTPB固体火箭推进剂启裂断裂韧性的试验测定[J].弹道学报,2012,24 (3): 96-99.
[9] Liu C T.Investigating the Constraint Effect in a Particulate Composite Material[R].ADA410745,2002.
[10] 常新龙,余堰峰,张有宏,等.HTPB推进剂老化断裂性能试验[J].推进技术,2011,32(4):364-368.(CHANG Xin-long,YU Yan-feng,ZHANG You-hong,et al.Testing on Aging Fracture Properties of HTPB Propellant[J].Journal of Propulsion Technology,2011,32 (4): 564-568.)
[11] Anderson T L.Fracture Mechanics,Fundamentals and Applications[M].Boca Raton: CRC Press,1995.
[12] Saouma V E,Natekar D,Hansen E.Cohesive Stress and Size Effects in Elasto-Plastic and Quasi-Brittle Materials[J].International Journal of Fracture,2003,119 (3):287-298.
[13] Smith W G,Liu C T.Global and Near Tip Response of Cracked Solid Propellant[R].ADA418742,1993.
[14] Liu C T,Smith W G.Near-Tip Behavior in a Particulate Material under Constant Strain Rate Including Temperate and Thickness Effects[R].ADA410504,2001.(编辑:朱立影)收稿日期:2013-11-02;修订日期:2013-12-10。作者简介:龙兵(1986—),男,博士生,研究领域为失效物理与可靠性。E-mail:longbingfh@126.com
|