陆春义.底排装置强非稳态燃烧特性研究[D].南京: 南京理工大学, 2009.LU Chun-yi.Study on characteristics of unstable combustion of base bleed unit[D].Nanjing: Nanjing University of Science and Technology,2009.
[3]
张领科, 周彦煌, 余永刚.底排装置工作不一致性对射程散布影响的研究[J].兵工学报, 2010,31(4): 442-446.ZHANG Ling-ke, ZHOU Yan-huang, YU Yong-gang.Research on range dispersion of base bleed projectile caused by inconsistent working characteristics of base bleed unit[J].Acta Armamentarii, 2010,31(4): 442-446.
[4]
金志明, 袁亚雄, 宋明.现代内弹道学[M].北京: 北京理工大学出版社, 1992.
[5]
郭锡福.底排药柱初温对射程的影响[J].兵工学报, 2003,24(2): 264-265.GUO Xi-fu.Effect of initial temperature of base bleed grain on its range[J].Acta Armamentarii, 2003,24(2): 264-265.
[6]
CAI Wei-dong, Thakre Piyush, YANG Vigor.A model of AP/HTPB composite propellant combustion in rocket-motor environments[J].Combustion Science and Technology, 2008,180: 2143-2169.
[7]
Kubota N, Miyazaki S.Temperaturesensitivity of burning rate of ammonium perchlorate propellants[J].Propellants, Explosive, Pyrotechnics, 1987,12: 183-187.
[8]
Sergey V, Charles A W.Kinetics of thermal decomposition of cubic ammonium perchlorate[J].Chem.Mater, 1999,11: 3386-3393.
[9]
Michael T G, John R O.Temperature sensitivity coefficients of solid propellant burning rate[J].Acta Astronautica, 1986,13(3): 127-130.
[10]
Click R L.Temperature sensitivity of solid propellant burning rate[J].AIAA Journal, 1967,5(3): 586-587.
[11]
Beckstead M W.Model for double-base propellant combustion[J].AIAA Journal, 1980,18(8): 980-985.
[12]
Beckstead M W, Derr R L, Price C F.The combustion of solid monopropellants and composite propellants[C]∥13th international symposium on combustion.1971: 1047-1056.
[13]
Cohen N S, Lo G A, Growley J C.Simplifications and variations of the Ben Reuven-Caveny Model of HMX combustion[C]∥18th JANNAF Combustion Meeting.1981: 361-372.
[14]
Beckstead M W.Combustion calculations for composite solide propellants[C]∥13th JANNAF Combustion Meeting.1976,299-312.
[15]
Coates R L.An analysis of simplified laminar flame theory for solid propellant combustion[J].Journal of Combustion Science and Technology, 1971,4(1):1-8.
[16]
Renie J P, Condon J A, Osborn J R.Oxidizer size distribution effects on propellant combustion[J].AIAA Journal, 1980,18(3): 277-293.
[17]
Cohen N S.Mechanisms and models of solid propellant burn rate temperature sensitivity-a review[R].AIAA, 1984.
[18]
Jacobs P W, Whitehead H M.Decomposition and combustion of ammonium perchlorate[J].Chemic Reviews, 1969,69(4): 551-590.
