[1] 邢耀国, 董可海, 沈伟,等.固体火箭发动机使用工程[M].北京:国防工业出版社, 2010.
[2] Copetti M IM, French D A.Numerical Solution of a Thermo-Viscoelastic Contact Problem by a Penalty Method[J].SIAM Journal on Numerical Analysis, 3,1(4):1487-1504.
[3] 杨挺青.粘弹性力学[M].武汉:华中理工大学出版社, 1990.
[4] 于洋, 王宁飞, 张平.温度载荷下带筋套管形装药结构完整性分析[J].推进技术, 6,7(6):493-496.(YU Yang, WANG Ning-fei, ZHANG Pin.Structural Integrity Analysis for the Canular Solid Propellant Grains Subjected to Temperature Loading[J].Journal of Propulsion Technology, 6,7(6):493-496.)
[5] Duncan E J S.A Nonlinear Viscoelastic Theory for Solid Rocket Propellants Based on a Cumulative Damage Approach[J].Propellants, Explosives, Pyrotechnics, 8,3(1):94-104．
[6] Heller R A,Singh M P.Thermal Storage Life of Solid-Propellant Motors[J].Spacecraft, 3,0(2):144-149.
[7] Heller R A, Singh M P, Zibdeh H.Environmental Effects on Cumulative Damage in Rocket Motors[J].Spacecraft, 5,2(2):149-155.
[8] 朱智春, 蔡峨.固体火箭发动机寿命评估的一种考虑[J].推进技术, 6,7(4):10-14.(ZHU Zhi-chun, CAI E.A Finite Element Analysis of Three Dimensional Temperature and Stress Fields for Solid Rocket Motor Grain[J].Journal of Propulsion Technology,6,7(4):10-14.)
[9] Richard K K.Continuum Damage Mechanics Modeling of Solid Propellant[C]. Hartford:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference,2008.
[10] HO S Y.High Strain-Rate Impact Studies of Predamaged Rocket Propellants I.Characterization of Damage Using a Cumulative Damage Failure Criterion[J].Combustion and Flame, 6,4(4):524-534.
[11] 邢耀国, 曲凯, 许俊松, 等.舰船摇摆条件下固体火箭发动机舰载寿命预估[J].推进技术, 1,2(1):32-35.(XING Yao-guo, QU Kai, XU Jun-song, et al.Life Prediction of Shipborne Solid Rocket Motor Under the Ship Swing Motion[J].Journal of Propulsion Technology, 1,2(1):32-35.)
[12] 李高春, 董可海, 张勇,等.环境温度载荷作用下固体火箭发动机药柱的累积损伤规律[J].火炸药学报, 0,3(4):19-22.
[13] Thangjitham S, Heller R A.Stress Response of Rocker Motors to Environmental Thermal Loads[J].J.Spacecraft,6,3(5):519-526.
|
