不同层状变燃速发射药药型的内弹道性能数值模拟

原浩1, 马中亮1*, 张世林1, 史伟伟1, 康润宇1, 陈春林2

化工新型材料 ›› 2023, Vol. 51 ›› Issue (3) : 185 -190.

PDF
化工新型材料 ›› 2023, Vol. 51 ›› Issue (3) : 185-190. DOI: 10.19817/j.cnki.issn1006-3536.2023.03.033
科学研究

不同层状变燃速发射药药型的内弹道性能数值模拟

    原浩1, 马中亮1*, 张世林1, 史伟伟1, 康润宇1, 陈春林2
作者信息 +

Numerical simulation of internal ballistic performance of different layered variable burning rate propellant

  • Yuan Hao1, Ma Zhongliang1, Zhang Shilin1, Shi Weiwei1, Kang Runyu1, Chen Chunlin2
Author information +
文章历史 +
PDF

摘要

为研究药型对层状变燃速发射药内弹道性能的影响,基于经典内弹道理论建立了多种药型的层状变燃速发射药物理燃烧模型,并推导计算了对应的形状函数与燃气生成猛度表达式,通过VC++软件对在定容条件下的不同药型的层状变燃速发射药内弹道性能进行了数值计算。结果表明:圆饼与方片层状变燃速发射药的燃烧性能相似,且比两面包覆的矩形变燃速发射药燃烧性能好;对于长方体变燃速发射药四面包覆比两面包覆的燃气生成猛度有明显的提高。在12.7mm枪装填条件下,长方体四面包覆比两面包覆膛内最大压力和弹丸初速分别降低11.94%和2.39%。

Abstract

In order to study the influence of propellant type on the internal ballistic performance of layered variable burning rate propellant,physical combustion models of various propellant types were established based on classical internal ballistic theory,and the corresponding shape function and gas generation intensity expression were deduced and calculated.By VC++ software,the internal ballistic performance of layered variable burning rate propellant under constant volume condition was numerically calculated.The results showed that the combustion performance of circular cake and square slice layered variable burning rate propellants was similar,and better than that of rectangular variable burning rate propellants covered on two sides.For cuboid propellant with variable burning rate,the gas generation fierceness of four shells was obviously higher than that of two shells.Under the loading condition of 12.7mm gun,the maximum pressure and muzzle velocity of cuboid four shells were 11.94% and 2.39% lower than those of two shells,respectively.

关键词

层状变燃速发射药 / 内弹道 / 燃烧性能 / 药型

Key words

layered variable burning rate propellant / internal ballistic / combustion performance / medicine type

引用本文

引用格式 ▾
不同层状变燃速发射药药型的内弹道性能数值模拟[J]. 化工新型材料, 2023, 51(3): 185-190 DOI:10.19817/j.cnki.issn1006-3536.2023.03.033

登录浏览全文

4963

注册一个新账户 忘记密码

参考文献

[1] 范雪坤,马忠亮,朱林.变燃速发射药燃烧性能研究进展[J].四川兵工学报,2011,32(7):48-50.
[2] 陆安舫.美国发射药装备特点及发展概况[J].火炸药,1983(6):26-31.
[3] 萧忠良,贺增弟,马忠亮,等.变燃速发射药的原理与实现方法[J].火炸药学报,2005,28(1):25-27.
[4] 廖静林,江劲勇,路桂娥,等.改善发射药燃烧性能的包覆物选择研究[J].化工新型材料,2011,39(5):127-129.
[5] Brown J J,Thynell S T,Kuo K K.Regression behavior of composite-layered gun propellants[M].Pennsylvania:Pennsylvania State University,1993.
[6] Robbins W.Continued studies of programmed-splitting stick propellant[P].US:AD-A188987,1982-10.
[7] Knott G,Brewster M Q.A two-dimensional model of composite propellent flame structure and burning rate[C].Las Vegas,NV,U.S.A.:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,2000.
[8] Luman B J R,Wehrman K K,Kuo R A,et al.Development and characterization of highperformance solid propellants containing nano-sized energetic ingredients[J].Proceedings of the Combustion Institute,2006,31(2):2089-2096.
[9] 马中亮,李志良,徐方亮,等.药型尺寸对变燃速发射药燃烧渐增性的影响[J].含能材料,2007,15(2):128-130.
[10] 鲁坤,马中亮,萧忠良.药型对层状发射药燃烧渐增性的影响[J].含能材料,2011,19(1):69-73.
[11] 钟建华,张丽华,萧忠良,等.方片状变燃速发射药燃气生成规律理论分析[J].含能材料,2010,18(5):579-582.
[12] 王率宇,马中亮,刘平.七孔变燃速发射药内孔位置对燃烧性能的影响[J].化工新型材料,2015,43(4):143-145.
[13] 马中亮,王率宇,刘平.七孔变燃速发射药参数对燃烧性能影响的研究[J].化工新型材料,2016,44(9):72-74,80.
[14] 张江波,张玉成,蒋树君.多层发射药内弹道模型及数值求解[J].火炸药学报,2009(3):83-86.
[15] 牛星星,梁家豪,吕敬伟,等.“三明治”片状发射药形状函数及燃烧性能计算[J].兵器装备工程学报,2019,40(1):68-73.
[16] 姚顺龙,张世林,白昌盛,等.片状变燃速发射药燃烧性能的数值计算[J].火炸药学报,2021,44(2):252-257.

基金资助

国防科技预先研究项目(40406020104)

AI Summary AI Mindmap
PDF

530

访问

0

被引

导航
相关文章

AI思维导图

/