基于膨胀波发射技术的火炮内弹道与发射动力学分析
|
摘要
本论文以新型高性能低后坐武器系统——膨胀波火炮为研究对象,针对膨胀波火炮的发射机理、后喷装置工作性能、内弹道过程数值仿真、发射性能分析及优化、发射身管振动响应及发射系统动力学特性等方面展开了研究。具体内容如下:
(1)针对膨胀波火炮核心组成部分——后喷装置的结构及工作性能进行了研究分析。根据膨胀波火炮的发射机理及实现过程给出了后喷装置的设计要求及可行的后喷打开方式;结合惯性炮尾后喷装置的工作原理,对其结构参数进行选取设定,并基于膨胀波传播理论给出了后喷打开时机的计算方法;建立了后喷流场的求解模型,全面分析了发射过程中不同后喷结构下燃气的后喷流动状态及后效作用范围,论证了不同结构后喷装置的工作性能。
(2)建立了膨胀波火炮一维两相流内弹道数学模型并进行数值仿真。分析了发射过程中内弹道各参量的变化规律,并同常规火炮内弹道过程进行对比计算,揭示了有别于常规火炮内弹道过程的特有的膛内射击现象;针对钝感发射药不同性能参数下的内弹道过程进行计算求解,分析了表层相对燃速系数、钝感层相对厚度以及药粒主要结构特征量等参数对内弹道性能的影响。与此同时,建立了前置喷孔膨胀波火炮双一维两相流内弹道数学模型并进行了数值求解分析,给出了发射过程中火炮膛内及导气管内各状态参量的变化规律,并分析了导气管结构参数及发射药性能对内弹道性能的影响。
(3)针对膨胀波火炮发射过程中的性能优势,对其发射性能进行研究分析及优化设计。建立了膨胀波火炮及常规闭膛火炮后坐力、后坐冲量、身管热量以及发射过程中发射药能量转换的计算公式,通过数值计算比对,验证了膨胀波火炮在减后坐、降低身管热量以及提高发射药实际利用率三方面的优越性能,并给出了包括装药量、药室容积、弹丸质量以及挤进压力在内的各装填条件,后喷打开时机以及后喷结构参数对发射性能的影响规律;在此基础上,综合膨胀波火炮发射性能的评价标准,建立了膨胀波火炮发射性能的多目标优化模型并给出了相应的求解方法,以装填密度及后喷打开时机为主要优化变量进行优化计算,给出满足各评价标准的可行方案。
(4)建立了膨胀波火炮身管振动响应的动力学方程并进行数值仿真。分析了发射过程中身管在膛内火药燃气、弹丸及惯性炮尾共同作用下的振动响应规律,给出了装填密度、弹丸质量、身管长度、后喷打开时机、惯性炮尾质量以及喷口截面扩张比等参数变化对身管振动响应的影响规律,并与常规发射过程下的振动响应进行了对比分析。在此基础上,给出了求解刚柔耦合系统动力学问题的建模方法,建立了膨胀波火炮发射系统整体动力学响应的刚柔耦合动力学模型并进行了数值求解,揭示了车体系统与发射身管间耦合作用的动力学特性。
The research is developed and aims at the new high performance weapon system------
Rarefaction Wave Gun(RAVEN). The propulsion mechanism of RAVEN, the structure design and working performance of blow back device, the numerical simulation of interior ballistic process, the research and optimization of propulsion performance, the vibration response and dynamic characteristics of gun are studied in this dissertation. The main parts are concluded as follows:
(1) The structure and working performance of the key part of RAVEN------blow backdevice is studied. The selection rule of blow back device and feasible venting method are given based on the propulsion mechanism and the realization processes of RAVEN. Combined with the working principle of the inertial breech blow back device, the structure parameters are made, and then the calculation method about the venting time is obtained by the rarefaction wave propagation theory as well. The calculation model of the venting flow field is established, the venting flow and aftereffect range of the propellant gas under the different structure of the blow back device are analyzed, and then the working performance of different blow back devices are verified.
(2) One-dimensional two-phase flow interior ballistics mathematical model of the RAVEN is established and its numerical simulations are conducted. The change laws of interior ballistic parameters are analyzed. The special firing phenomenon is given by comparing calculation with the conventional close-breech gun. The rules of how the surface relative burning-rate coefficient, relative thickness of the deterred layer and main structure characteristic parameter of deterred propellant grain effect on the interior ballistic performance are made by calculation. Meanwhile the dual one-dimensional two-phase flow interior ballistics mathematical model of the Front Orifice Rarefaction Wave Gun is established and its numerical simulations are conducted. The change laws of interior ballistic parameters in the bore and airway are obtained and the effect on the interior ballistic performance of structure parameters of the airway and deterred propellant performance is analyzed.
(3) The analysis and optimization design about the propulsion performance of the Rarefaction Wave Gun is developed for its unique performance advantages. The calculation formulas about recoil force, recoil impulse, barrel heat and energy conversion in the propulsion of Rarefaction Wave Gun and the conventional close-breech gun are established. By the numerical calculation, the performances of the Rarefaction Wave Gun in the reducing the recoil and barrel heat and increasing practical efficiency of propellant are verified. The rules how the different loading conditions including the loading charge mass, chamber volume, projectile mass and engraving pressure, the venting time and the structure parameters of blow back device affect on the performance are obtained. On this basis, the multi-object optimization model of the propulsion performance of the Rarefaction Wave Gun is established and the corresponding solving method is given by combining the corresponding evaluation standards of the propulsion performance. Make the loading density and the venting time as the main optimization variables, the feasible project are made out to satisfy different evaluation criterion by the calculation.
(4) The dynamic vibration equation of the Rarefaction Wave Gun is established and its numerical simulations are conducted. The vibration responses in the action of the propellant gas, projectile and the inertial breech are obtained. The rules of how the different parameters including the loading density, projectile mass, barrel length, venting time , inertial breech mass and the expansion ratio of nozzle section effect on the vibration response is given. Comparing calculation with the vibration response of the conventional closed-breech gun, the specific vibration phenomenon is also obtained. The modeling method about the dynamic problem of the rigid-flexible coupling system is given, and then the rigid-flexible coupling dynamic model that describes the whole dynamic response of the Rarefaction Wave Gun system is established and its numerical simulations are conducted. The dynamic characteristics of the coupling effect between body system and gun barrel is given.
(1)针对膨胀波火炮核心组成部分——后喷装置的结构及工作性能进行了研究分析。根据膨胀波火炮的发射机理及实现过程给出了后喷装置的设计要求及可行的后喷打开方式;结合惯性炮尾后喷装置的工作原理,对其结构参数进行选取设定,并基于膨胀波传播理论给出了后喷打开时机的计算方法;建立了后喷流场的求解模型,全面分析了发射过程中不同后喷结构下燃气的后喷流动状态及后效作用范围,论证了不同结构后喷装置的工作性能。
(2)建立了膨胀波火炮一维两相流内弹道数学模型并进行数值仿真。分析了发射过程中内弹道各参量的变化规律,并同常规火炮内弹道过程进行对比计算,揭示了有别于常规火炮内弹道过程的特有的膛内射击现象;针对钝感发射药不同性能参数下的内弹道过程进行计算求解,分析了表层相对燃速系数、钝感层相对厚度以及药粒主要结构特征量等参数对内弹道性能的影响。与此同时,建立了前置喷孔膨胀波火炮双一维两相流内弹道数学模型并进行了数值求解分析,给出了发射过程中火炮膛内及导气管内各状态参量的变化规律,并分析了导气管结构参数及发射药性能对内弹道性能的影响。
(3)针对膨胀波火炮发射过程中的性能优势,对其发射性能进行研究分析及优化设计。建立了膨胀波火炮及常规闭膛火炮后坐力、后坐冲量、身管热量以及发射过程中发射药能量转换的计算公式,通过数值计算比对,验证了膨胀波火炮在减后坐、降低身管热量以及提高发射药实际利用率三方面的优越性能,并给出了包括装药量、药室容积、弹丸质量以及挤进压力在内的各装填条件,后喷打开时机以及后喷结构参数对发射性能的影响规律;在此基础上,综合膨胀波火炮发射性能的评价标准,建立了膨胀波火炮发射性能的多目标优化模型并给出了相应的求解方法,以装填密度及后喷打开时机为主要优化变量进行优化计算,给出满足各评价标准的可行方案。
(4)建立了膨胀波火炮身管振动响应的动力学方程并进行数值仿真。分析了发射过程中身管在膛内火药燃气、弹丸及惯性炮尾共同作用下的振动响应规律,给出了装填密度、弹丸质量、身管长度、后喷打开时机、惯性炮尾质量以及喷口截面扩张比等参数变化对身管振动响应的影响规律,并与常规发射过程下的振动响应进行了对比分析。在此基础上,给出了求解刚柔耦合系统动力学问题的建模方法,建立了膨胀波火炮发射系统整体动力学响应的刚柔耦合动力学模型并进行了数值求解,揭示了车体系统与发射身管间耦合作用的动力学特性。
The research is developed and aims at the new high performance weapon system------
Rarefaction Wave Gun(RAVEN). The propulsion mechanism of RAVEN, the structure design and working performance of blow back device, the numerical simulation of interior ballistic process, the research and optimization of propulsion performance, the vibration response and dynamic characteristics of gun are studied in this dissertation. The main parts are concluded as follows:
(1) The structure and working performance of the key part of RAVEN------blow backdevice is studied. The selection rule of blow back device and feasible venting method are given based on the propulsion mechanism and the realization processes of RAVEN. Combined with the working principle of the inertial breech blow back device, the structure parameters are made, and then the calculation method about the venting time is obtained by the rarefaction wave propagation theory as well. The calculation model of the venting flow field is established, the venting flow and aftereffect range of the propellant gas under the different structure of the blow back device are analyzed, and then the working performance of different blow back devices are verified.
(2) One-dimensional two-phase flow interior ballistics mathematical model of the RAVEN is established and its numerical simulations are conducted. The change laws of interior ballistic parameters are analyzed. The special firing phenomenon is given by comparing calculation with the conventional close-breech gun. The rules of how the surface relative burning-rate coefficient, relative thickness of the deterred layer and main structure characteristic parameter of deterred propellant grain effect on the interior ballistic performance are made by calculation. Meanwhile the dual one-dimensional two-phase flow interior ballistics mathematical model of the Front Orifice Rarefaction Wave Gun is established and its numerical simulations are conducted. The change laws of interior ballistic parameters in the bore and airway are obtained and the effect on the interior ballistic performance of structure parameters of the airway and deterred propellant performance is analyzed.
(3) The analysis and optimization design about the propulsion performance of the Rarefaction Wave Gun is developed for its unique performance advantages. The calculation formulas about recoil force, recoil impulse, barrel heat and energy conversion in the propulsion of Rarefaction Wave Gun and the conventional close-breech gun are established. By the numerical calculation, the performances of the Rarefaction Wave Gun in the reducing the recoil and barrel heat and increasing practical efficiency of propellant are verified. The rules how the different loading conditions including the loading charge mass, chamber volume, projectile mass and engraving pressure, the venting time and the structure parameters of blow back device affect on the performance are obtained. On this basis, the multi-object optimization model of the propulsion performance of the Rarefaction Wave Gun is established and the corresponding solving method is given by combining the corresponding evaluation standards of the propulsion performance. Make the loading density and the venting time as the main optimization variables, the feasible project are made out to satisfy different evaluation criterion by the calculation.
(4) The dynamic vibration equation of the Rarefaction Wave Gun is established and its numerical simulations are conducted. The vibration responses in the action of the propellant gas, projectile and the inertial breech are obtained. The rules of how the different parameters including the loading density, projectile mass, barrel length, venting time , inertial breech mass and the expansion ratio of nozzle section effect on the vibration response is given. Comparing calculation with the vibration response of the conventional closed-breech gun, the specific vibration phenomenon is also obtained. The modeling method about the dynamic problem of the rigid-flexible coupling system is given, and then the rigid-flexible coupling dynamic model that describes the whole dynamic response of the Rarefaction Wave Gun system is established and its numerical simulations are conducted. The dynamic characteristics of the coupling effect between body system and gun barrel is given.
引文
1 Frank H.Armament systems & technologies for the FCS/Object force.National Defense Industrial Association,Virginia,2001
2 Josef S.Future combat systems.National Defense Industrial Association,Virginia,2001
3 周永生,张肖斌.战场新锐:FCS美陆军未来战斗系统.国防科技,2005(6):22-28
4 华菊仙,岳松堂.“未来战斗系统”的关键技术-“渡鸦”膨胀波火炮技术.现代兵器,2004(8):8-10
5 岳松堂,华菊仙.“渡鸦”--将对未来战斗系统产生重大影响的膨胀波火炮.外军炮兵,2004(8):17-20
6 Dunn S,Witherell M,Sopok S,et al.Rarefaction wave gun propulsion.U.S.Army ARDEC Close Combat Armaments Center,New Jersey,2001
7 Dillon R,Kathe E.Sonic rarefaction wave low recoil gun.U.S.Army ARDEC Close Combat Armaments Center,New Jersey,2002
8 王靖君,赫信鹏.火炮概论.第1版.北京:兵器工业出版社,1992
9 高树滋,陈运生,郑建国等.火炮反后坐装置设计.第1版.北京:兵器工业出版社,1995
10 Kern L TG,Paul J.Future combat systems.21st Systems and Technology Symposium.The Defense Advanced Research Projects Agency,Dallas,2000
11 Zahn C B.The future combat system:minimizing risk while maximizing capability.USAWC Strategy Research Project,USA,2000
12 Yalamanchili R.New concepts in recoil mechanisms.U.S.Army ARDEC Large callber weapon systems laboratory,New Jersey,1980
13 Gast R,Kathe E.A fire out-of-battery tank gun:theory and simulation.U.S.Army ARDEC Ben(?)t Laboratories,New York,2002
14 张志坚.前冲式反后坐装置设计研究.南京:南京理工大学,2007
15 杨军荣.基于软后坐技术的某自动迫击炮动力学分析.弹道学报,2006(1):63-67
16 高树滋,郑建国.可压缩液体技术反后坐装置的原理和应用.兵工学报,1993(4):64-68
17 谈乐斌,侯保林,陈卫民.降低火炮后坐力技术概述.火炮发射与控制学报,2006(4):69-72
18 Pengelley R.LTHD-a lightweight hope for rapid deployment artillerymen.International Defense Review,1998(2):145-148
19 何永,高树滋.火炮曲线后坐动力学分析与研究.火炮发射与控制学报,1994(3):35-39
20 何永,杨军荣,高树滋.曲线后坐火炮后坐阻力规律的分析与研究.南京理工大学学 报,1997(3):217-220
21 高树滋,何永.一种轻型牵引炮的新型后坐系统.火炮发射与控制学报,1997(1):52-57
22 何永,郑建国,高树滋.二维后坐火炮分析及摇架设计.火炮发射与控制学报,2000(2):43-46
23 吴承缢,张莺.无后坐炮设计.第1版.北京:兵器工业出版社,1994
24 Headquarter,U.S.Army Material Command.Recoilless rifle weapon system.AMCP706-238,Washington,1976
25 彭焕新.平衡炮的计算与研究.南京:南京理工大学,2003
26 Czysz P A.Solid propellant 75mm recoilless gun system for airborne applications.U.S.Army,TACOM-ARDEC Ben(?)t Laboratories,Watervliet,New York,2002
27 Kathe E.Recoil reduction using propellant gas.U.S.Army,TACOM-ARDEC Ben(?)t Laboratories,Watervliet,New York,2003
28 邱凤昌,张月林译.炮口装置.第1版.北京:国防工业出版社,1974
29 李鸿志.炮口装置受力与效率计算.南京理工学学报,1984(3):1-17+7-8
30 李鸿志,崔东明,何正求等.高膛压滑膛炮炮口制退器的设计特点及性能评价指标.南京理工大学学报,1994(5):22-24
31 廖振强,李永新,孔德仁等.一种新的膛口装置正交设计优化方法.兵工学报,2000(2):97-100
32 江坤.炮口制退器优化设计理论与方法研究.南京:南京理工大学,2007
33 Krieger I M,Collins E A.Electrorhelolgical fluids:a research needs assessment.Washington:Government Printing Office DC,1993
34 姚国治,孟光,方周.电流变液的性能及其应用研究.力学进展,1996(4):521-531
35 Rupert P.Towed artillery advances.Tane's International Defense Review,1988(4):35-42
36 童睆,王国辉,松刚等.电流变液体在火炮反后坐装置上的应用.火炮发射与控制学报,2006(S1):108-111
37 王国辉,高雷,刘云泉.基于电流变液的火炮反后坐技术研究.装甲兵工程学院学报,2006(1):37-39
38 Kathe E.Sonic Rarefaction wave recoilless gun system.United States Patent:6460446B1,2002-10-8
39 Kathe E,Nagamastsu H,Flaherty J.New gun shakes up FCS.U.S.Army,TACOM-ARDEC Ben(?)t Laboratories,New York,2003
40 金志明.枪炮内弹道学.第1版.北京:北京理工大学出版社,2004
41 金志明,袁亚雄,宋明.现代内弹道学.第1版.北京:北京理工大学出版社,1992
42 Kuo K K,Koo J H.Transient combustion in granular propellant beds.Part Ⅰ:Theoretical modeling and numerical solution of transient combustion processes in mobile granular propellant beds.Pennsylvania State University Park Department of Mechanical Engineering, Pennsylvania, 1977
43 Kuo K K, Davis T R.Transient combustion in granular propellant beds.Part Ⅱ:experiment study of transient combustion processes in mobile granular propellant beds.Pennsylvania State University Park Department of Mechanical Engineering,Pennsylvania, 1977
44 Gough P S.The predictive capacity of models of interior ballistics.Proceedings of the 12th JANNAF Combustion Meeting, CPIA, 1975
45 Gough P S.Zwarts F J.Modeling heterogeneous two-phase reacting flow.AIAA/SAE 13th Propulsion Conference, Oralndo, Florida, 1977
46 Gough P S.Two dimensional convective flamespreading in packed beds of granular propellant.USA Armament Research and Development Command Ballistic Research Laboratory, Maryland, 1979
47 Krier H, Summerfield M.Interior ballistics of guns.Isd ed.American Institute of Aeronautics and Astronautics, New York, 1979
48 Kulkami A R, Dalai K S, Sharma K C.A study on pressure variation in a turbulent flow.17th International Symposium on Ballistics.Midrand, South Africa, 1998:491-499
49 Gough P S.The XNOVAKTC code.U.S.Army BRL-CR-627, Paul Gough Associates,Portsmouth, New Hampshire, 1990
50 Gough P S.Interior ballistics modeling: extensions to the one-dimensional XKTC code and analytical studies of pressure gradient for lumped parameter codes.Army Research Laboratory, Maryland, 2001
51 Sakamoto K, Matsunaga K.Numerical analysis of the propagating blast wave in a firing range.19th International Symposium on Ballistics, Interlaken, Switzerland,2001:289-296
52 Lasjsewa D.Two-dimensional modeling of propellant ignition by a plasma jet.17th International Symposium on Ballistics, Midrand, South Africa, 1998:456-461
53 Nusca M J.Computational fluid dynamics model of multiphase flows applied to solid propellant combustion in gun system.18th International Symposium on Ballistics, San Antonio, Texas, USA, 2000:252-261
54 Woodley C R.Comparison pf 0D and ID interior ballistics modeling of high performance direct fire guns.19th International Symposium on Ballistics, Interlaken, Switzerland, 2001:57-64
55 Du Toit P S.Two-dimensional interior ballistics model for modular solid propellant charges.19th International Symposium on Ballistics, Interlaken, Switzerland, 2001:89-98
56 Woodley C R.Modeling the internal ballistics of mortars using the one-dimensional code CTA1.20th International Symposium on Ballistics, Orlando, Florida, USA,2002:274-282
57 Kuo K K, Moore J D.Characterization of the M1020 ignition cartridge under simulated mortar firing conditions.21st International Symposium on Ballistics, Adelaide, Australia,2004:582-588
58 Luke G, Eagar M, Sears M et al.Status of advanced two-phase flow model development for SRM chamber flow and combustion modeling.Aerojet Sacramento, California, 2004
59 Nusca M J, Horst A W.Progress in modeling ignition in a solid propellant charge for telescoped ammunition.U.S.Army Research Laboratory Weapons and Materials Research Directorate, Maryland, 2005
60 Woodley C, Carriere A.Comparisons of internal ballistics simulations of the agard gun.22nd International Symposium on Ballistics, Vancouver, British Columbia, Canada,2005:338-345
61 Cayzac R, Carette E.Unstady Intermediate Ballistics: 2D and 3D CFD modelig application to sabot sepation.22nd International Symposium on Ballistics, Vancouver,British Columbia, Canada, 2005:398-404
62 Horst A W, Conroy P J.Flame-spreading process in a small-caliber gun.U.S.Army Research Laboratory Weapons and Materials Research Directorate, Maryland, 2007
63 Schmidt J R.Nusca Michael.Investigation of small-caliber primer function using a multiphase computational model.U.S.Army Research Laboratory Weapons and Materials Research Directorate, Maryland, 2008
64 Kathe E, Dillon R E.Sonic rarefaction wave low recoil gun.In: American Institute of Aeronautics and Astronautics.39th Aerospace Sciences Meeting & Exhibit, Reno,Nevada, 2001: 1-10
65 Navaz H K, Dang A D.Numerical analysis of bipropellant combustion in liquid thrust chambers by an Eulerian-Eulerian approach.In: American Institute of Aeronautics and Astronautics.28th Joint Propulsion Conference and Exhibit, Nashville, Tennessee, 1992:1-10
66 Hartern A.High resolution scheme for hyperbolic conservation law.Journal of Computational Physics, 1997(2):260-278
67 Navaz H K, Dunn S.A computer model for gun barrel flow analysis: the gun tube boundary layer code(GTBL).Software and Engineering Associates,Carson City,1999
68 Dunn S,French J,Coats D et al.Internal ballistics analysis for raven propulsion system.U.S.Army,TACOM-ARDEC Ben(?)t Laboratories,New Yory,2001
69 Kathe E.Rarefaction wave gun propulsion.New York:Rensselaer Polytechnic Institute,2002
70 Anderson R D,Fickle K D.IBHVG2-A user's guide.U.S.Army Ballistic Research Laboratory,Maryland,1987
71 Gough P S.Initial development of core module of next generation interior ballistic model NGEN.U.S.Army Ballistic Research Laboratory,Maryland,1995
72 Coffee T P.A two-dimensional model for the combustion chamber/gun tube of a concept VIC regenerative liquid propellant gun.U.S.Army Ballistic Research Laboratory,Maryland,1992
73 Peterkin R E,Frese M H,Sovinec C R.Transport of magnetic flux in an arbitrary coordinate ALE code.Journal of Computational Physics,1998(1):148-171
74 Coffee T P.Modeling of the 35-mm rarefaction wave gun.U.S.Army Research Laboratory,Maryland,2006
75 周彦煌,王升晨.实用两相流内弹道学.第1版.北京:兵器工业出版社,1990
76 袁亚雄,张小兵.高温高压多相流体动力学基础.第1版.哈尔滨:哈尔滨工业大学出版社,2005
77 周彦煌,王升晨.中心点火管装药结构两相流内弹道模型及计算.兵工学报,1987(4):12-21
78 周彦煌,刘千里,王升晨.底部点火结构两相流内弹道模型及计算.兵工学报,1989(1):4-11
79 刘千里,王升晨,张明安.中心点火结构三维两相流内弹道数值模拟.火炮发射与控制学报,1996(3):1-9
80 翁春生,袁亚雄,金志明.管状发射药内弹道模型及计算.弹道学报,1993(3):1-7
81 翁春生,袁亚雄,金志明.开槽管状药内弹道模型及计算.弹道学报,1993(4):14-19
82 翁春生,袁亚雄,金志明.一种复杂装药结构的两相流内弹道模型及计算.南京理工大学学报,1995(5):297-301
83 张小兵,翁春生,袁亚雄.混合颗粒床中颗粒轨道模型及其数值模拟.工程力学,1998(2):129-137
84 张小兵,袁亚雄,金志明.分装式高装填密度火炮轴对称两维多相流数值模拟.兵工学报,1998(1):10-15
85 陆欣,周彦煌,余永刚.整装式液体随行装药的两相流数值仿真.兵工学报, 2001(1):27-30
86 陆中兵,周彦煌.模块装药火炮内弹道两维两相流数值预测.兵工学报,2001(3):298-301
87 翁春生,金志明,袁亚雄.大口径榴弹炮多相流内弹道数值预报.南京理工大学学报,1997(5):407-410
88 张小兵,彭振伟,王力等.串联双药室火炮经典内弹道模型及数值模拟.南京理工大学学报,1999(2):101-104
89 申越,袁亚雄,张小兵.超高射频武器系统的内弹道一维两相流数值仿真.兵工学报,2005(5):600-604
90 倪志军,周克栋,郝雷.非常规结构武器两相流内弹道的高精度数值模拟.爆炸与冲击,2006(5):468-473
91 徐流恩,李永池,高乐南.大口径高速平衡炮发射安全性分析.中国科学技术大学学报,2008(11):1304-1310
92 张帆,廖振强,王涛等.膨胀波枪炮发射原理数值建模与分析.南京理工大学学报,2007(1):17-21
93 张帆,廖振强,刘国鑫等.膨胀波枪炮发射性能若干影响因素的研究.兵工学报,2008(1):23-27
94 张帆,廖振强,刘国鑫等.喷孔前置式膨胀波枪炮发射过程数值仿真与分析.系统仿真学报,2008(18):5032-5305
95 张帆.膨胀波火炮发射原理及其在常规结构枪炮中的应用.南京:南京理工大学,2008
96 支建庄,郑坚,狄长春等.膨胀波火炮膨胀波速度和行程的数值模拟.军械工程学院学报,2008(4):39-42
97 芮筱亭.多体系统发射动力学研究.南京:南京理工大学,1993
98 Langhaar H L,Miller R E,Boresi A P.Excitation of a gun barrel due to firing.2nd US Army Symposium on Gun Dynamics,Part Ⅰ,Rensselaerville,New York,1978:34-57
99 Chu S H.In-bore motion analysis of XM712 projectile in the M198 gun.ARLCD-TR-80005,ARDC,Dover,New Jersey,1980
100 Cox P A,Hokanson J C.Muzzle motion of the M68 105mm Gun.2nd US Army Symposium on Gun Dynamics,Part Ⅰ,Rensselaerville,New York,1978:18-33
101 Cox P A.Hokanson J C.The influence of tube support conditions on muzzle motions.U.S.Army Research Office Research Triangle Park,North Carolina,1982
102 Simkins T E.Transverse response of gun tubes to curvature-induced load functions.2nd US Army Symposium on Gun Dynamics,Part Ⅰ,Rensselaerville,New York,1978:58-66
103 Sneck H J.Cast R.Normal mode analysis of gun tube dynamics.4th US Army Symposium on Gun Dynamics,Part Ⅰ,Riviera Beach,Florida,1985:21-50
104 Soifer M T and Recker R S.In-bore projectile motions.4th US Army Symposium on Gun Dynamics,Part Ⅱ,Riviera Beach,Florida,1985:70-88
105 Simkins T E.Resonance of flexural waves in gun tubes.5th U S Army Symposium on Gun Dynamics,PartⅠ,Rensselaerville,New York,1987:64-78
106 康新中,王宝元.炮管振动的有限元分析.兵工学报,1990(2):16-22
107 王宝元.移动弹丸作用下的炮管振动.兵工学报武器分册,1990(2):6-15
108 周叮,谢玉树.弹丸膛内运动引起炮管振动的小参数解法.振动与冲击,1999(1):76-81
109 骆文润,王德石.火炮身管横向振动分析.非线性动力学学报,2001(3):239-244
110 于海龙,芮筱亭,何斌等.火炮身管固有振动特性的有限元传递矩阵法.弹道学报,2006(3):62-64
111 姜沐,郭锡福.弹丸加速运动在身管中激发的振动.弹道学报,2002(3):57-63
112 胡红生.移动质量激励梁振动主动控制研究.南京:南京理工大学,2005
113 Kane T R.Multi-body dynamics.Journal of Applied Mechanics,1983(4):1071-1078
114 Huston R L.Kane's equations with undetermined multipliers-application on constrained multi-body systems.Journal of Applied Mechanics,1987(2):424-429
115 刘延柱,洪嘉振,杨海兴等.多刚体系统动力学.第1版.北京:高等教育出版社,1989
116 Boresi A P,Langhaar H L.Dynamics of rigid guns with straight tubes.US Army Armament Research and Development Command,Aberdeen Proving Ground,Maryland,1983
117 Philip D.Benzkofer M R.Automated dynamic analysis of weapon systems.4th US Army Symposium on Gun Dynamics,Part Ⅱ,Riviera Beach,Florida,1985:89-108
118 何永,高树滋.考虑身管柔性的火炮多体动力学方法.南京理工大学学报,1995(4):302-307
119 康新中.多体理论及其在火炮工程中的应用前景.火炮发射与控制学报,1996(4):7-12
120 敖勇,陈运生,毛保全.火炮多体系统动力学分析的一种方法.弹道学报,1997(4):19-22
121 陈运生,杨国来.自行火炮动力学的Kane方法建模研究.火炮发射与控制学报,1995(1):1-5
122 陈运生,敖勇,毛保全.自行火炮动力学分析的一种广义模态综合法.弹道学报,1997(1):31-34
123 杨国来,杨军荣,陈运生.某自动迫击炮动力学参数影响规律研究.弹道学报,2004(1):19-23
124 闵建平.自行火炮行进间发射动力学研究.南京:南京理工大学,2001
125 钱明伟,王良明.自行火炮行进间动力学模型及仿真研究.兵工学报,2004(5):520-524
126 石明全.某火炮自动供输弹系统和全跑耦合的发射动力学研究.南京:南京理工大学,2003
127 冯勇,马大为,薛畅等.多管火箭炮刚柔耦合多体发射动力学仿真研究.兵工学报,2006(3):545-548
128 时爱民,苏铭德,刘季稔.气体动力学基础.第1版.北京:科学出版社,1986
129 王福军.计算流体动力学分析--CFD软件原理与应用.第1版.北京:清华大学出版社,2004
130 易文俊,汤瑞峰.钝感发射药的内弹道特性研究.南京理工大学学报,1997(2):133-136
131 陆家鹏,谭兴良,雷志义.自动武器气体动力学.第1版.北京:兵器工业出版社,1991
132 陶其恒.涉及身管传热的膛内流动及其计算.南京理工大学学报,1997(1):21-24
133 胡敏达.多目标规划有效性理论.第1版.上海:上海科学技术出版社,1994
134 施光燕,董加礼.最优化方法.第1版.北京:高等教育出版社,1999
135 魏世孝,周献中.多属性决策理论方法及其在C3I系统中的应用.第1版.北京:国防工业出版社,1998
136 郭锡福.弹丸发射动力学.第1版.南京:华东工学院,1988
137 欧阳光耀,王树宗,王德石.火炮身管振动特性及减振研究.海军工程学院学报,1999(2):79-86
138 马春茂.高炮结构参数对炮口振动影响的分析.兵工学报武器分册,1992(2):30-33
139 欧阳光耀,王树宗,王德石.火炮身管振动吸振的原理与实验研究.南京理工大学学报,1999(5):409-413
140 章定国,肖建强.一个刚柔耦合的火箭发射架动力学模型.应用数学和力学,2005(5):561-568
141 余继邦,章定国.考虑“动力刚化”的刚柔耦合多体系统动力学建模的子系统法.南京理工大学学报,2006(4):409-413
142 Cai G P,Hong J Z,Yang S X.Dynamics analysis of a flexible hub-beam system with tip mass.Mechanics Research Communications,2005(2):173-190
143 康新中,吴三灵,马春茂等.火炮系统动力学.第1版.北京:国防工业出版社,1999
2 Josef S.Future combat systems.National Defense Industrial Association,Virginia,2001
3 周永生,张肖斌.战场新锐:FCS美陆军未来战斗系统.国防科技,2005(6):22-28
4 华菊仙,岳松堂.“未来战斗系统”的关键技术-“渡鸦”膨胀波火炮技术.现代兵器,2004(8):8-10
5 岳松堂,华菊仙.“渡鸦”--将对未来战斗系统产生重大影响的膨胀波火炮.外军炮兵,2004(8):17-20
6 Dunn S,Witherell M,Sopok S,et al.Rarefaction wave gun propulsion.U.S.Army ARDEC Close Combat Armaments Center,New Jersey,2001
7 Dillon R,Kathe E.Sonic rarefaction wave low recoil gun.U.S.Army ARDEC Close Combat Armaments Center,New Jersey,2002
8 王靖君,赫信鹏.火炮概论.第1版.北京:兵器工业出版社,1992
9 高树滋,陈运生,郑建国等.火炮反后坐装置设计.第1版.北京:兵器工业出版社,1995
10 Kern L TG,Paul J.Future combat systems.21st Systems and Technology Symposium.The Defense Advanced Research Projects Agency,Dallas,2000
11 Zahn C B.The future combat system:minimizing risk while maximizing capability.USAWC Strategy Research Project,USA,2000
12 Yalamanchili R.New concepts in recoil mechanisms.U.S.Army ARDEC Large callber weapon systems laboratory,New Jersey,1980
13 Gast R,Kathe E.A fire out-of-battery tank gun:theory and simulation.U.S.Army ARDEC Ben(?)t Laboratories,New York,2002
14 张志坚.前冲式反后坐装置设计研究.南京:南京理工大学,2007
15 杨军荣.基于软后坐技术的某自动迫击炮动力学分析.弹道学报,2006(1):63-67
16 高树滋,郑建国.可压缩液体技术反后坐装置的原理和应用.兵工学报,1993(4):64-68
17 谈乐斌,侯保林,陈卫民.降低火炮后坐力技术概述.火炮发射与控制学报,2006(4):69-72
18 Pengelley R.LTHD-a lightweight hope for rapid deployment artillerymen.International Defense Review,1998(2):145-148
19 何永,高树滋.火炮曲线后坐动力学分析与研究.火炮发射与控制学报,1994(3):35-39
20 何永,杨军荣,高树滋.曲线后坐火炮后坐阻力规律的分析与研究.南京理工大学学 报,1997(3):217-220
21 高树滋,何永.一种轻型牵引炮的新型后坐系统.火炮发射与控制学报,1997(1):52-57
22 何永,郑建国,高树滋.二维后坐火炮分析及摇架设计.火炮发射与控制学报,2000(2):43-46
23 吴承缢,张莺.无后坐炮设计.第1版.北京:兵器工业出版社,1994
24 Headquarter,U.S.Army Material Command.Recoilless rifle weapon system.AMCP706-238,Washington,1976
25 彭焕新.平衡炮的计算与研究.南京:南京理工大学,2003
26 Czysz P A.Solid propellant 75mm recoilless gun system for airborne applications.U.S.Army,TACOM-ARDEC Ben(?)t Laboratories,Watervliet,New York,2002
27 Kathe E.Recoil reduction using propellant gas.U.S.Army,TACOM-ARDEC Ben(?)t Laboratories,Watervliet,New York,2003
28 邱凤昌,张月林译.炮口装置.第1版.北京:国防工业出版社,1974
29 李鸿志.炮口装置受力与效率计算.南京理工学学报,1984(3):1-17+7-8
30 李鸿志,崔东明,何正求等.高膛压滑膛炮炮口制退器的设计特点及性能评价指标.南京理工大学学报,1994(5):22-24
31 廖振强,李永新,孔德仁等.一种新的膛口装置正交设计优化方法.兵工学报,2000(2):97-100
32 江坤.炮口制退器优化设计理论与方法研究.南京:南京理工大学,2007
33 Krieger I M,Collins E A.Electrorhelolgical fluids:a research needs assessment.Washington:Government Printing Office DC,1993
34 姚国治,孟光,方周.电流变液的性能及其应用研究.力学进展,1996(4):521-531
35 Rupert P.Towed artillery advances.Tane's International Defense Review,1988(4):35-42
36 童睆,王国辉,松刚等.电流变液体在火炮反后坐装置上的应用.火炮发射与控制学报,2006(S1):108-111
37 王国辉,高雷,刘云泉.基于电流变液的火炮反后坐技术研究.装甲兵工程学院学报,2006(1):37-39
38 Kathe E.Sonic Rarefaction wave recoilless gun system.United States Patent:6460446B1,2002-10-8
39 Kathe E,Nagamastsu H,Flaherty J.New gun shakes up FCS.U.S.Army,TACOM-ARDEC Ben(?)t Laboratories,New York,2003
40 金志明.枪炮内弹道学.第1版.北京:北京理工大学出版社,2004
41 金志明,袁亚雄,宋明.现代内弹道学.第1版.北京:北京理工大学出版社,1992
42 Kuo K K,Koo J H.Transient combustion in granular propellant beds.Part Ⅰ:Theoretical modeling and numerical solution of transient combustion processes in mobile granular propellant beds.Pennsylvania State University Park Department of Mechanical Engineering, Pennsylvania, 1977
43 Kuo K K, Davis T R.Transient combustion in granular propellant beds.Part Ⅱ:experiment study of transient combustion processes in mobile granular propellant beds.Pennsylvania State University Park Department of Mechanical Engineering,Pennsylvania, 1977
44 Gough P S.The predictive capacity of models of interior ballistics.Proceedings of the 12th JANNAF Combustion Meeting, CPIA, 1975
45 Gough P S.Zwarts F J.Modeling heterogeneous two-phase reacting flow.AIAA/SAE 13th Propulsion Conference, Oralndo, Florida, 1977
46 Gough P S.Two dimensional convective flamespreading in packed beds of granular propellant.USA Armament Research and Development Command Ballistic Research Laboratory, Maryland, 1979
47 Krier H, Summerfield M.Interior ballistics of guns.Isd ed.American Institute of Aeronautics and Astronautics, New York, 1979
48 Kulkami A R, Dalai K S, Sharma K C.A study on pressure variation in a turbulent flow.17th International Symposium on Ballistics.Midrand, South Africa, 1998:491-499
49 Gough P S.The XNOVAKTC code.U.S.Army BRL-CR-627, Paul Gough Associates,Portsmouth, New Hampshire, 1990
50 Gough P S.Interior ballistics modeling: extensions to the one-dimensional XKTC code and analytical studies of pressure gradient for lumped parameter codes.Army Research Laboratory, Maryland, 2001
51 Sakamoto K, Matsunaga K.Numerical analysis of the propagating blast wave in a firing range.19th International Symposium on Ballistics, Interlaken, Switzerland,2001:289-296
52 Lasjsewa D.Two-dimensional modeling of propellant ignition by a plasma jet.17th International Symposium on Ballistics, Midrand, South Africa, 1998:456-461
53 Nusca M J.Computational fluid dynamics model of multiphase flows applied to solid propellant combustion in gun system.18th International Symposium on Ballistics, San Antonio, Texas, USA, 2000:252-261
54 Woodley C R.Comparison pf 0D and ID interior ballistics modeling of high performance direct fire guns.19th International Symposium on Ballistics, Interlaken, Switzerland, 2001:57-64
55 Du Toit P S.Two-dimensional interior ballistics model for modular solid propellant charges.19th International Symposium on Ballistics, Interlaken, Switzerland, 2001:89-98
56 Woodley C R.Modeling the internal ballistics of mortars using the one-dimensional code CTA1.20th International Symposium on Ballistics, Orlando, Florida, USA,2002:274-282
57 Kuo K K, Moore J D.Characterization of the M1020 ignition cartridge under simulated mortar firing conditions.21st International Symposium on Ballistics, Adelaide, Australia,2004:582-588
58 Luke G, Eagar M, Sears M et al.Status of advanced two-phase flow model development for SRM chamber flow and combustion modeling.Aerojet Sacramento, California, 2004
59 Nusca M J, Horst A W.Progress in modeling ignition in a solid propellant charge for telescoped ammunition.U.S.Army Research Laboratory Weapons and Materials Research Directorate, Maryland, 2005
60 Woodley C, Carriere A.Comparisons of internal ballistics simulations of the agard gun.22nd International Symposium on Ballistics, Vancouver, British Columbia, Canada,2005:338-345
61 Cayzac R, Carette E.Unstady Intermediate Ballistics: 2D and 3D CFD modelig application to sabot sepation.22nd International Symposium on Ballistics, Vancouver,British Columbia, Canada, 2005:398-404
62 Horst A W, Conroy P J.Flame-spreading process in a small-caliber gun.U.S.Army Research Laboratory Weapons and Materials Research Directorate, Maryland, 2007
63 Schmidt J R.Nusca Michael.Investigation of small-caliber primer function using a multiphase computational model.U.S.Army Research Laboratory Weapons and Materials Research Directorate, Maryland, 2008
64 Kathe E, Dillon R E.Sonic rarefaction wave low recoil gun.In: American Institute of Aeronautics and Astronautics.39th Aerospace Sciences Meeting & Exhibit, Reno,Nevada, 2001: 1-10
65 Navaz H K, Dang A D.Numerical analysis of bipropellant combustion in liquid thrust chambers by an Eulerian-Eulerian approach.In: American Institute of Aeronautics and Astronautics.28th Joint Propulsion Conference and Exhibit, Nashville, Tennessee, 1992:1-10
66 Hartern A.High resolution scheme for hyperbolic conservation law.Journal of Computational Physics, 1997(2):260-278
67 Navaz H K, Dunn S.A computer model for gun barrel flow analysis: the gun tube boundary layer code(GTBL).Software and Engineering Associates,Carson City,1999
68 Dunn S,French J,Coats D et al.Internal ballistics analysis for raven propulsion system.U.S.Army,TACOM-ARDEC Ben(?)t Laboratories,New Yory,2001
69 Kathe E.Rarefaction wave gun propulsion.New York:Rensselaer Polytechnic Institute,2002
70 Anderson R D,Fickle K D.IBHVG2-A user's guide.U.S.Army Ballistic Research Laboratory,Maryland,1987
71 Gough P S.Initial development of core module of next generation interior ballistic model NGEN.U.S.Army Ballistic Research Laboratory,Maryland,1995
72 Coffee T P.A two-dimensional model for the combustion chamber/gun tube of a concept VIC regenerative liquid propellant gun.U.S.Army Ballistic Research Laboratory,Maryland,1992
73 Peterkin R E,Frese M H,Sovinec C R.Transport of magnetic flux in an arbitrary coordinate ALE code.Journal of Computational Physics,1998(1):148-171
74 Coffee T P.Modeling of the 35-mm rarefaction wave gun.U.S.Army Research Laboratory,Maryland,2006
75 周彦煌,王升晨.实用两相流内弹道学.第1版.北京:兵器工业出版社,1990
76 袁亚雄,张小兵.高温高压多相流体动力学基础.第1版.哈尔滨:哈尔滨工业大学出版社,2005
77 周彦煌,王升晨.中心点火管装药结构两相流内弹道模型及计算.兵工学报,1987(4):12-21
78 周彦煌,刘千里,王升晨.底部点火结构两相流内弹道模型及计算.兵工学报,1989(1):4-11
79 刘千里,王升晨,张明安.中心点火结构三维两相流内弹道数值模拟.火炮发射与控制学报,1996(3):1-9
80 翁春生,袁亚雄,金志明.管状发射药内弹道模型及计算.弹道学报,1993(3):1-7
81 翁春生,袁亚雄,金志明.开槽管状药内弹道模型及计算.弹道学报,1993(4):14-19
82 翁春生,袁亚雄,金志明.一种复杂装药结构的两相流内弹道模型及计算.南京理工大学学报,1995(5):297-301
83 张小兵,翁春生,袁亚雄.混合颗粒床中颗粒轨道模型及其数值模拟.工程力学,1998(2):129-137
84 张小兵,袁亚雄,金志明.分装式高装填密度火炮轴对称两维多相流数值模拟.兵工学报,1998(1):10-15
85 陆欣,周彦煌,余永刚.整装式液体随行装药的两相流数值仿真.兵工学报, 2001(1):27-30
86 陆中兵,周彦煌.模块装药火炮内弹道两维两相流数值预测.兵工学报,2001(3):298-301
87 翁春生,金志明,袁亚雄.大口径榴弹炮多相流内弹道数值预报.南京理工大学学报,1997(5):407-410
88 张小兵,彭振伟,王力等.串联双药室火炮经典内弹道模型及数值模拟.南京理工大学学报,1999(2):101-104
89 申越,袁亚雄,张小兵.超高射频武器系统的内弹道一维两相流数值仿真.兵工学报,2005(5):600-604
90 倪志军,周克栋,郝雷.非常规结构武器两相流内弹道的高精度数值模拟.爆炸与冲击,2006(5):468-473
91 徐流恩,李永池,高乐南.大口径高速平衡炮发射安全性分析.中国科学技术大学学报,2008(11):1304-1310
92 张帆,廖振强,王涛等.膨胀波枪炮发射原理数值建模与分析.南京理工大学学报,2007(1):17-21
93 张帆,廖振强,刘国鑫等.膨胀波枪炮发射性能若干影响因素的研究.兵工学报,2008(1):23-27
94 张帆,廖振强,刘国鑫等.喷孔前置式膨胀波枪炮发射过程数值仿真与分析.系统仿真学报,2008(18):5032-5305
95 张帆.膨胀波火炮发射原理及其在常规结构枪炮中的应用.南京:南京理工大学,2008
96 支建庄,郑坚,狄长春等.膨胀波火炮膨胀波速度和行程的数值模拟.军械工程学院学报,2008(4):39-42
97 芮筱亭.多体系统发射动力学研究.南京:南京理工大学,1993
98 Langhaar H L,Miller R E,Boresi A P.Excitation of a gun barrel due to firing.2nd US Army Symposium on Gun Dynamics,Part Ⅰ,Rensselaerville,New York,1978:34-57
99 Chu S H.In-bore motion analysis of XM712 projectile in the M198 gun.ARLCD-TR-80005,ARDC,Dover,New Jersey,1980
100 Cox P A,Hokanson J C.Muzzle motion of the M68 105mm Gun.2nd US Army Symposium on Gun Dynamics,Part Ⅰ,Rensselaerville,New York,1978:18-33
101 Cox P A.Hokanson J C.The influence of tube support conditions on muzzle motions.U.S.Army Research Office Research Triangle Park,North Carolina,1982
102 Simkins T E.Transverse response of gun tubes to curvature-induced load functions.2nd US Army Symposium on Gun Dynamics,Part Ⅰ,Rensselaerville,New York,1978:58-66
103 Sneck H J.Cast R.Normal mode analysis of gun tube dynamics.4th US Army Symposium on Gun Dynamics,Part Ⅰ,Riviera Beach,Florida,1985:21-50
104 Soifer M T and Recker R S.In-bore projectile motions.4th US Army Symposium on Gun Dynamics,Part Ⅱ,Riviera Beach,Florida,1985:70-88
105 Simkins T E.Resonance of flexural waves in gun tubes.5th U S Army Symposium on Gun Dynamics,PartⅠ,Rensselaerville,New York,1987:64-78
106 康新中,王宝元.炮管振动的有限元分析.兵工学报,1990(2):16-22
107 王宝元.移动弹丸作用下的炮管振动.兵工学报武器分册,1990(2):6-15
108 周叮,谢玉树.弹丸膛内运动引起炮管振动的小参数解法.振动与冲击,1999(1):76-81
109 骆文润,王德石.火炮身管横向振动分析.非线性动力学学报,2001(3):239-244
110 于海龙,芮筱亭,何斌等.火炮身管固有振动特性的有限元传递矩阵法.弹道学报,2006(3):62-64
111 姜沐,郭锡福.弹丸加速运动在身管中激发的振动.弹道学报,2002(3):57-63
112 胡红生.移动质量激励梁振动主动控制研究.南京:南京理工大学,2005
113 Kane T R.Multi-body dynamics.Journal of Applied Mechanics,1983(4):1071-1078
114 Huston R L.Kane's equations with undetermined multipliers-application on constrained multi-body systems.Journal of Applied Mechanics,1987(2):424-429
115 刘延柱,洪嘉振,杨海兴等.多刚体系统动力学.第1版.北京:高等教育出版社,1989
116 Boresi A P,Langhaar H L.Dynamics of rigid guns with straight tubes.US Army Armament Research and Development Command,Aberdeen Proving Ground,Maryland,1983
117 Philip D.Benzkofer M R.Automated dynamic analysis of weapon systems.4th US Army Symposium on Gun Dynamics,Part Ⅱ,Riviera Beach,Florida,1985:89-108
118 何永,高树滋.考虑身管柔性的火炮多体动力学方法.南京理工大学学报,1995(4):302-307
119 康新中.多体理论及其在火炮工程中的应用前景.火炮发射与控制学报,1996(4):7-12
120 敖勇,陈运生,毛保全.火炮多体系统动力学分析的一种方法.弹道学报,1997(4):19-22
121 陈运生,杨国来.自行火炮动力学的Kane方法建模研究.火炮发射与控制学报,1995(1):1-5
122 陈运生,敖勇,毛保全.自行火炮动力学分析的一种广义模态综合法.弹道学报,1997(1):31-34
123 杨国来,杨军荣,陈运生.某自动迫击炮动力学参数影响规律研究.弹道学报,2004(1):19-23
124 闵建平.自行火炮行进间发射动力学研究.南京:南京理工大学,2001
125 钱明伟,王良明.自行火炮行进间动力学模型及仿真研究.兵工学报,2004(5):520-524
126 石明全.某火炮自动供输弹系统和全跑耦合的发射动力学研究.南京:南京理工大学,2003
127 冯勇,马大为,薛畅等.多管火箭炮刚柔耦合多体发射动力学仿真研究.兵工学报,2006(3):545-548
128 时爱民,苏铭德,刘季稔.气体动力学基础.第1版.北京:科学出版社,1986
129 王福军.计算流体动力学分析--CFD软件原理与应用.第1版.北京:清华大学出版社,2004
130 易文俊,汤瑞峰.钝感发射药的内弹道特性研究.南京理工大学学报,1997(2):133-136
131 陆家鹏,谭兴良,雷志义.自动武器气体动力学.第1版.北京:兵器工业出版社,1991
132 陶其恒.涉及身管传热的膛内流动及其计算.南京理工大学学报,1997(1):21-24
133 胡敏达.多目标规划有效性理论.第1版.上海:上海科学技术出版社,1994
134 施光燕,董加礼.最优化方法.第1版.北京:高等教育出版社,1999
135 魏世孝,周献中.多属性决策理论方法及其在C3I系统中的应用.第1版.北京:国防工业出版社,1998
136 郭锡福.弹丸发射动力学.第1版.南京:华东工学院,1988
137 欧阳光耀,王树宗,王德石.火炮身管振动特性及减振研究.海军工程学院学报,1999(2):79-86
138 马春茂.高炮结构参数对炮口振动影响的分析.兵工学报武器分册,1992(2):30-33
139 欧阳光耀,王树宗,王德石.火炮身管振动吸振的原理与实验研究.南京理工大学学报,1999(5):409-413
140 章定国,肖建强.一个刚柔耦合的火箭发射架动力学模型.应用数学和力学,2005(5):561-568
141 余继邦,章定国.考虑“动力刚化”的刚柔耦合多体系统动力学建模的子系统法.南京理工大学学报,2006(4):409-413
142 Cai G P,Hong J Z,Yang S X.Dynamics analysis of a flexible hub-beam system with tip mass.Mechanics Research Communications,2005(2):173-190
143 康新中,吴三灵,马春茂等.火炮系统动力学.第1版.北京:国防工业出版社,1999