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1.
叙述了调试57mm一级气体炮中所遇到的问题和解决方法,调试发射的结果为:发射管长7.92m,气室容积0.018m^3在9MPa空气介质时,可使280g弹这到460m/s出口速度,注入18MPa氢气时,可使280g弹丸达到900m/s出口速度。  相似文献   

2.
对比实验表明,利用与等离子体发生器联结的中空管结构从弹丸底部点燃推进剂,不仅可以提高弹丸的出口动通顺学能降低膛内的压力;如果单纯依靠增加电源系统的初始电能提高弹丸的出口动能,其副作用是增加了膛内压力。研究结果表明,推进剂点火结构的合理设计对提高电热化学炮的发射效率有重要意义。  相似文献   

3.
本文描述了三种不同密度(0.6,0.76和0.9g/cm ̄3)的环氧树脂-SiO_2空心微球复合材料的Hugoniot关系。讨论了上述材料以其相应的Hugoniot关系作为参考方程的Mie-Gruneisen方程,并与P-α模型进行了比较,结果相当一致。由此得出结论,在本文研究的压力范围内,Mie-Gruneisen方程可应用于上述孔隙材料。  相似文献   

4.
本文描述了三种不同密度(0.6,0.76和0.9g/cm ̄3)的环氧树脂-SiO_2空心微球复合材料的Hugoniot关系。讨论了上述材料以其相应的Hugoniot关系作为参考方程的Mie-Gruneisen方程,并与P-α模型进行了比较,结果相当一致。由此得出结论,在本文研究的压力范围内,Mie-Gruneisen方程可应用于上述孔隙材料。  相似文献   

5.
本文介绍了电热炮的基本原理、实验装置结构、等离子体发生器和发射实验结果。实验结果表明,电热炮原理实验的装置是成功的,已将19.3g复合弹丸加速到1.85km/s,穿透30mm厚的钢板。  相似文献   

6.
采用通光式传感法和直接测量特定时间间隔的探头原理,在闪光2号装置上进行了电子束辐照硬铝靶产生的喷射冲量耦合系数与能通量关系的研究。结果表明:在能通量为115~240J/cm2范围内,喷射冲量和亏损质量面密度都随能通量近似线性变化,而喷射冲量耦合系数随能通量增大而缓慢递增,并趋于一渐近值;硬铝产生喷射冲量的能通量阈值为40J/cm2左右;喷射冲量值为81~218Pas,亏损质量面密度为3.1 10-2~8.610-2g/cm2,喷射冲量耦合系数为0.70~0.98Pas/(J/cm 2)。  相似文献   

7.
输沙量(率)水平分布的非均一性   总被引:13,自引:0,他引:13  
凌裕泉 《实验力学》1994,9(4):352-356
实验表明:输沙率沿风洞实验段横截面的水平分布具有明显的非均一性。其正负距平变幅可达平均值的45-60%。输沙率与有效起沙风成正比关系,其实验式为q=8.95×10(-1)(VL-Vt)(1.9)(g/cm·min),Vt=5.0m/s。与Bagnold,RA理论公式q=8.70×10(-2)(V-Vt)3相比(Vt=4.0m/s),前者计算结果更接近室内外实测值。  相似文献   

8.
本文以水空气两相流体为工质,研究了两相流体横向冲刷准三角形柱体时的涡街生成特性,试验段管子内径50mm,水流速度2.20m/s-7.74m/s,截面含气率为0.02-0.3。得出了两相流中涡街发生频率,水流量和截面含气率三者之间的相互关系。  相似文献   

9.
本文以水空气两相流体为工质,研究了两相流体横向冲刷准三角形柱体时的涡街生成特性.试验段管子内径50mm,水流速度2.20m/s-3.74m/s截面含气率为0.02-0.3.得出了两相流体中涡街发生频率,水流量和截面含气率三者之间的相互关系。  相似文献   

10.
复合材料正交叠层板最终拉伸强度的细观统计分析   总被引:8,自引:0,他引:8  
曾庆敦  马锐  范赋群 《力学学报》1994,26(4):451-461
本文对复合材料正交叠层板[0/90/0]的最终拉伸破坏行为进行了研究.首先,提出一种修正的剪滞分析方法,求解叠层中由90°层的基体开裂和0°层的部分纤维断裂相互作用所导致的应力重新分布;然后,采用随机临界核统计模型,对叠层板的最终破坏进行了细观统计分析.对[O_2/90_m]_s、[O_4/90_m]_s碳/环氧和[O_4/90_m]_s玻璃/环氧的计算结果表明,估计的最终拉伸强度与现有的实验结果有较好的符合.  相似文献   

11.
The electroexplosive and electrothermal mechanisms and the principles of conduction and induction electrodynamics are used simultaneously to convert electromagnetic energy to the kinetic energy of projectiles. This approach is implemented on the basis of the well–known configuration of a coaxial pinch accelerator. It is established that there is an active lengths of the barrel on which the system ensures launching with nearly constant acceleration. For a barrel length of 340 mm and a barrel diameter of 17 mm, bodies with a mass of 1—12 g are accelerated to velocities of 3.4—1.45 km/sec with an energy conversion efficiency of 25—29% at a capacitive storage voltage of 1.75 kV and a discharge current of up to 150 kA. Bodies with a mass of 40—80 g (barrel diameter 25 mm are accelerated to velocities of 1.3—1.0 km/sec with an efficiency of 28—20% at a voltage of 3.5 kV and a current of up to 220 kA.  相似文献   

12.
为研究结构弹体对钢筋混凝土靶的高速侵彻破坏效应,利用口径35 mm弹道炮开展了1 030~1 520 m/s速度范围内的高速侵彻试验,获得了弹体的撞击速度、破坏形态、剩余长度、剩余质量和靶体中的侵彻深度及成坑尺寸等试验数据,分析了侵彻深度和侵彻机理随速度的变化关系。结果表明:在1 030~1 390 m/s的速度范围内,弹体头部磨蚀,磨蚀程度随侵彻速度增加而加剧,侵彻深度随撞击速度近似线性增大;撞击速度在1 390~1 480 m/s范围内,弹体头部严重磨蚀,侵彻深度随撞击速度增加而减小;撞击速度大于1 480 m/s后,弹体严重破碎,侵彻深度急剧下降。针对结构弹体高速侵彻过程中的破坏特点,将侵彻速度划分为刚体侵彻区、准刚体侵彻区、侵蚀体侵彻区和破碎体侵彻区,可为钻地弹结构设计提供参考。  相似文献   

13.
The operation of rapid burst firing multirail electromagnetic launchers of solids is numerically simulated using unsteady two-dimensional and three-dimensional models. In the calculations, the launchers are powered by a Sakhalin pulsed magnetohydrodynamic generator. Launchers with three and five pairs of parallel rails connected in a series electrical circuit are considered. Firing sequences of different numbers of solid projectiles of different masses is modeled. It is established that the heating of the rails is one of the main factors limiting the performance of launchers under such conditions. It is shown that the rate of heating of the rails is determined by the nonuniformity of the current density distribution over the rail cross-section due to the unsteady diffusion of the magnetic field into the rails. Calculations taking into account the unsteady current density distribution in the rails of a multirail launcher show that with an appropriate of the mass of the projectiles (up to 800 g), their number in the sequence, and the material of the rails, it is possible to attain launching velocities of 1.8–2.5 km/s with moderate heating of the rails.  相似文献   

14.
超高速撞击实验的三级压缩气炮技术   总被引:1,自引:0,他引:1  
介绍了弹速8km/s、氮气驱动三级压缩气炮技术的研究背景。论述了以三级压缩替代二级压缩 在提高氮气驱动多级气炮上限弹速方面的意义。讨论了弹径10mm 的57-37-10三级气炮的驱动气压、泵管 初充气压与发射弹速及高压气室荷载之间的关系。简述了57-37-10三级压缩气炮主要部件的工程设计,通 过实验数据和实物照片表述了57-37-10三级压缩气炮研究工作的进展情况。  相似文献   

15.
This paper describes the results of experimental studies on penetration of cylindrical projectiles into concrete and reinforced concrete at impact velocities reaching 0.5 km/s. An algorithm is proposed for calculating the depth of penetration of a projectile, making it possible to find the depth of penetration of high-strength steel projectiles with a mass of up to 13.5 kg into concrete on the basis of measurements of the specific work required to remove concrete using projectiles with a mass of up to 8 g.  相似文献   

16.
在理论分析的基础上 ,结合实验条件建立了液体发射药电热化学发射内弹道一维两相流数学模型 ,该模型包含电弧等离子体生成和运动、等离子体卷吸液体发射药生成小液滴以及膛内多相流体的相互作用。利用该模型对电热化学发射内弹道过程进行了数值模拟 ,并将模拟结果与实验数据进行了分析比较 ,结果表明模拟结果与实验数据基本吻合。  相似文献   

17.
王马法  周智炫  黄洁  罗庆  龙耀  焦德志  柳森 《爆炸与冲击》2021,41(5):053302-1-053302-9
为获得10 km/s超高速撞击成坑特性,采用内爆发射器开展了长径比l/dp为1/2、直径dp为0.8 cm的镁合金弹丸撞击厚5 cm铝靶的超高速撞击实验,获得了铝靶的撞击成坑尺寸和形貌特性,结合文献数据,分析了成坑形貌与8 km/s以下速度撞击坑的差异和弹丸长径比、速度、动能对成坑尺寸的影响。结果表明:典型的撞击坑不仅包含中心成坑区,还包含了破坏区,成坑区近似半球形弹坑,破坏区为自由表面剥落形成的浅坑;坑深Pc/dp为1.5~2.0,坑径dc/dp为3~3.5,坑形系数Pc/dc为0.50,成坑效率E/Vc均值为3.74 kJ/cm3;对于l/dp≤1的弹丸,采用等效直径对坑深进行归一化,归一化后坑深与长径比无关,与速度的2/3次幂成线性关系。  相似文献   

18.
弹体高速入水特性实验研究   总被引:4,自引:0,他引:4  
进行了速度在35~160 m/s的平头、卵形和截卵形弹体入水实验,利用高速相机记录了弹体入水和空泡扩展的详细过程,得到了3种弹体在入水初期的水中弹道轨迹和空泡形状,并比较分析了弹体头部形状对入水弹道稳定性的影响.结果表明,平头弹体在水中飞行有良好的弹道稳定性,截卵形弹体往往由于受力不均衡在入水后期发生偏转,卵形弹体则在...  相似文献   

19.
Yang  Huawei  Zhang  Jie  Wang  Zhiyong  Wang  Zhihua  Li  Q. M. 《Acta Mechanica Sinica》2021,37(3):482-493

A study on the resistance of rigid projectiles penetrating into semi-infinite concrete targets is performed in this paper. Experimental data are analyzed to examine the penetration resistance during various stages of the penetration process. A numerical tool using AUTODYN hydrocode is applied in the study. The numerical results on both deceleration-time history and depth of penetration of projectiles are in good agreement with experimental data, which demonstrate the feasibility of the numerical model in these conditions. Based on the numerical model with a two-staged pre-drilled hole, the rigid projectile penetration in tunneling stage is studied for concrete targets with different strengths in a wide range of impact velocities. The results show that the penetration in tunnel stage can be divided into two different cases in terms of initial impact velocity. In the first case, when the impact velocity is approximately less than 600 m/s, the deceleration depends on initial impact velocity. In the second case, when the impact velocity is greater than 600 m/s, the effect of target inertia becomes apparent, which agrees with commonly used concrete penetration resistance equations based on cavity expansion model.

Graphic abstract

A two-staged pre-drilled hole model was developed and the results show that the depth of entrance stage tends to decrease with the increase of impact velocity. The influence of the inertial term at low velocity range (approximately close to 600 m/s) is inconspicuous. With further increase of the penetration velocity, the effect of the target inertia becomes apparent as proposed by Forrestal. The effect of mass abrasion of projectiles, entrance phase and strain effect of concrete materials on the tendency of deceleration was clarified.

  相似文献   

20.
为研究椭圆截面弹体侵彻混凝土靶规律,基于动态球形空腔膨胀理论,建立椭圆截面弹体侵彻受力模型,计算典型椭圆截面弹体阻力规律和侵彻砂浆靶深度。在此基础上,采用弹道炮发射平台,开展相同质量和长度的2种典型椭圆截面弹体及圆截面弹体垂直侵彻半无限砂浆靶实验。结果表明:理论模型能够反映椭圆截面弹体受力情况,并与实验研究结果吻合较好;椭圆截面弹体长短轴参数的改变对侵彻性能影响较为显著。  相似文献   

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