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二级轻气炮内弹道的数值模拟与性能分析 被引量:3

NUMERICAL SIMULATION AND PERFORMANCE ANALYSIS OF THE TWO-STAGE LIGHT GAS GUN
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摘要 为了优化二级轻气炮的设计参数和工作参数,必须进行数值模拟。本文介绍了准一维不定常流的Lagrangian算法,讨论了数值模拟中的若干问题,分析了气动过程。根据我们的数值模拟,归纳了影响气炮性能的一些基本规律,可供选择工作参数时综合分析。 In order to optimize the performance of the two-stage gas gun, the initial--boundary value problems for quasi-one-dimensional unsteady flow are solved by difference method. The influence of operating parameters on the performance is as follows: (1) The opening pressure for rupture valve between breech and pump tube influences the use degree of the gun powder. (2) The increase of the opening pressure for rupture valve between the pump tube and barrel leads to a small increase in calculation projectile velocity and essentially increase in the stresses in the pump tube.(3) In view of large inertia, heavy piston can not undergo slowing down guickly. resulting in higher stresses in the tapered section (4) The projectile velocity does not increase monotonically with piston velocity in certain range of the piston velocity. (5) At the appropriate initial filled pressure. the maximum projectile velocity is not correspondence to maximum stress in the tapered section.
作者 陈大年
出处 《爆炸与冲击》 EI CAS CSCD 北大核心 1989年第1期37-42,共6页 Explosion and Shock Waves
关键词 二级轻气炮 弹道 数值模拟 性能 two-stage light gas gun, numerical simulation, performance analysis.
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参考文献1

  • 1陈大年,中国力学学会第二届液体力学学术会论文集,1983年

同被引文献16

  • 1吴应湘,郑之初,P.Kupschus.二级轻气炮发射性能的数值模拟[J].中国科学(A辑),1995,25(4):374-384. 被引量:2
  • 2林俊德.非火药驱动的二级轻气炮的发射参数分析[J].爆炸与冲击,1995,15(3):229-240. 被引量:13
  • 3管小荣,徐诚.二级轻气炮发射过程数学模型和计算方法[J].南京理工大学学报,2007,31(1):22-26. 被引量:5
  • 4GROTH C P T,GOTTLIEB J J.Numerical study of two-stage light-gas hypervelocity projectile launchers[R].Toronto:University of Toronto Intsitute for Aerospace Studies,1988.
  • 5BOGDANOFF D W,MILLER R J.New higher-order Godunov code for modelling performance of two-stage light gas guns[R].Washington D C:NASA,1995.
  • 6BOGDANOFF D W.Optimization study of the Ames 0.5" two-stage light gas gun[J].International Journal of Impact Engineering,1997,20:131-142.
  • 7BOGDANOFF D W,MILLER R J.Optimization study of the Ames 1.5" two-stage light gas gun[C].the 34th Aerospace Sciences Meeting and Exhibit.Reno,Nevada,1996.
  • 8魏叔如,蔡尔华.二级轻气炮性能的近似计算方法[J].力学与实践,1982,4(3):47-52.
  • 9JOHNSTON I A.The noble-abel equation of state:thermodynamic derivations for ballistics modelling[R].Edinburgh,South Australia,Australia:Defence Science and Technology Organisation,2005.
  • 10ZHOU L,ZHOU Y P.Determination of compressibility factor and fugacity coefficient of hydrogen in studies of adsorptive storage[J].International Journal of Hydrogen Energy,2001,26:597-601.

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