共查询到18条相似文献,搜索用时 108 毫秒
1.
2.
高速侵彻弹体的弹载部件/关键元器件的生存性与可靠性考核是引战系统研制领域的热点与难点问题,受原型试验的成本限制,利用缩比弹体搭载原型引信部件开展非等比例缩比试验研究是可行途径。针对传统等比例缩比方案无法满足弹体刚体过载相似性要求的情况,研究了非等比例缩比侵彻/贯穿相似规律,提出了非等比例缩比侵彻试验设计方法。数值计算结果表明:侵彻半无限厚混凝土靶条件下,非等比例缩比弹刚体过载的脉宽、幅值均可实现与原型弹刚体过载一致的加载条件;贯穿多层薄靶的条件下,通过调节靶板布置及弹体初速等试验工况,合理设计缩比弹体结构,可使非等比例缩比试验的弹体刚体过载峰值和脉宽覆盖原型试验。通过缩比模型试验得到的刚体过载特性可以为弹体及引信部件抗过载防护设计提供可靠的参考依据。 相似文献
3.
为了给侵彻引信抗高过载优化设计提供准确的力学输入,将机械振动理论引入侵彻过程建模领域,提出了一种侵彻战斗部刚体运动与一阶轴向振动相结合的垂直侵彻弹靶作用模型。在垂直侵彻过程受力分析的基础上,基于牛顿第二定律建立了战斗部刚体运动模型,基于单自由度弹簧-质量-阻尼系统建立了战斗部一阶轴向振动模型,并采用数值积分的方法获得了垂直侵彻过程中各物理量的变化规律。和火炮试验实测加速度信号的对比分析结果表明:考虑战斗部一阶轴向振动后的垂直侵彻弹靶作用模型能更准确地描述侵彻过程,能更有效地指导侵彻引信的抗高过载优化设计。 相似文献
4.
混凝土复合靶基体靶板的层数和中间粘结层厚度是复合靶能否模拟单一靶的两个重要影响因
素, 利用AUTODYN2D仿真软件, 重点研究了这两个因素对弹体侵彻过载的影响. 首先通
过已有的实验和理论公式验证了初始仿真模型和材料参数的合理性. 在此基础上, 通过改变
基体靶板的层数和中间粘结层厚度建立了多组侵彻复合靶的仿真算例. 通过弹体侵彻速度、
过载曲线的对比, 结果表明: 全尺寸深侵彻过载实验中复合靶能够代替单一靶, 但复合靶中
间粘结层的厚度不要大于1/2弹头部长度; 当中间粘结层厚度超过弹头部长度1/2时, 弹体
侵彻复合靶过载与侵彻单一靶的偏离程度随基体靶板层数的增加而增大, 上述结论可为实验
中构建混凝土复合靶提供参考. 相似文献
5.
为考核战斗部引信用火工品中起爆药的抗过载性能及适应性,通过火炮实弹射击的混凝土靶侵彻过载模拟实验,分析了典型起爆药在模拟弹中真实的力学环境、失效特性及承载能力。测试与计算结果表明:实验弹丸过载8.7×104g、脉宽持续时间约2 ms、最大速度708 m/s、侵彻深度0.57 m、起爆药惯性载荷最大瞬态作用力为85.34 N、冲量70.17 mN·s、最大瞬态作用能为0.466 8 J、总能量18.656 1 J。在此力学环境下,由于起爆药质量较小,实际承受加速度引起的作用力较小,与静态撞击感度测试作用势能数量级相当,起爆药在实验弹中未发现损伤。 相似文献
6.
7.
8.
通过Φ57mm半穿甲弹对钢筋混凝土的垂直侵彻实验,得到了弹丸的撞靶速度、成坑深度、最大侵彻深度以及过载时程曲线等实验数据.对实验后钢筋的断裂特征进行分析,得到钢筋的典型破坏模式.将钢筋的破坏简化为弯曲+剪切断裂和弯曲+拉伸断裂这两种模式.根据混凝土侵彻模型和梁断裂失效理论,建立了刚性弹丸垂直侵彻钢筋混凝土的简化分析模型.将理论计算得到的侵彻深度、速度与过载时间历程分别与实验数据进行对比,结果表明两者吻合较好.研究表明,钢筋只对弹体侵彻过程产生局部影响,混凝土的抗侵彻阻力仍是钢筋混凝土抗侵彻阻力的主要组成部分. 相似文献
9.
10.
弹体侵彻混凝土的临界跳弹 总被引:1,自引:0,他引:1
为了保证钻地战斗部打击防护层目标时不发生跳弹,需要对弹体侵彻目标的临界跳弹角度进行分析和估算。开展了一定大长径比弹体斜侵彻混凝土的跳弹实验,分析了在250~430 m/s速度下弹体侵彻30和60 MPa钢筋混凝土的临界跳弹角度,给出了弹体临界跳弹角度包络线。当靶板强度相同时,随着侵彻速度的增加,弹体的临界跳弹倾角增大,增大的趋势逐渐变缓;在相同侵彻速度下,随着靶板强度的增加,弹体的临界跳弹倾角减小;经验公式分析得到的弹体临界跳弹倾角偏低于实验,但偏差基本在3°以内。 相似文献
11.
The present paper presents a new experimental method to measure the deceleration time history of projectiles penetrating into
concrete in full-size test. The experiment can be carried out by using an onboard accelerometer to measure the projectile
deceleration history and the data are transmitted to a ground recording system. With this experimental method, a series of
tests on hemisphere-nose steel projectiles penetrating normally into plain concrete at the velocity region 150–400 m/s have
been executed and the deceleration histories obtained. The high frequency portion in the deceleration data has been investigated
and proved to be the structure response of projectile. The characteristics of deceleration history have also been analyzed
and discussed. 相似文献
12.
Based on the dynamic cavity-expansion theory and momentum theorem, the key parameters of projectile penetrating into concrete target, i.e., the penetration time and time histories of DOP, deceleration, mass loss, instant mass loss rate and nose shape, are obtained by incremental calculation considering mass loss of projectile. The calculation results are consistent with the experimental results. Due to the mass loss and thus nose blunting effects, the pulse shape of deceleration may be quite different from that obtained in the analysis of a rigid projectile, and then the dissimilarity is analyzed. It is found that the pulse shape of deceleration is determined by the drag force and essentially determined by the performances of target and projectile, i.e., the shear strength of target, the Moh’s hardness of aggregate in concrete and the CRH value of projectile nose. Further analysis indicates that the pulse shape of deceleration is more sensitive to the performance of target than that of projectile. 相似文献
13.
针对理想长杆侵彻,通过对长杆侵彻Alekseevskii-Tate模型近似解进行分析,指出单一的无量纲速度衰减系数α(deceleration index)不足以完全表征长杆高速侵彻的准定常阶段。在此基础上,重新定义了2个无量纲特征参量:Johnson破坏数ΦJp和特征时间系数β,2个参量之间的关系为α=β/ΦJp。分析表明,ΦJp和β(或α和β)可实现对长杆高速侵彻准定常阶段的弹尾速度的完全表征;若再引入长杆弹相对临界速度vc*,则可完全表征长杆侵彻的准定常阶段。此外,还证明了α能够判定侵彻过程偏离定常状态的程度,并指出通过确定ΦJp和β(或α和β),可针对攻防需求对长杆弹侵彻设计进行指导。 相似文献
14.
弹体侵彻与贯穿有限厚度混凝土靶体的力学特性 总被引:1,自引:0,他引:1
为了便于研究弹体贯穿混凝土靶体的力学本质,首先假设钻地弹是刚性弹体。在水动力侵彻模型的基础上,认为在弹体的冲击下,靶体裂缝扩展到靶体背面时就开始不稳定增长。将此时刻作为贯穿的发生时刻,据此利用裂缝增长的耗能机制求得了发生贯穿时,裂缝距靶体背面的临界距离。在求解贯穿发生后的侵彻阻抗力时考虑了由于靶体背面贯穿块的运动而造成的弹体相对速度的降低。计算表明,弹体端部侵入靶体与贯穿发生后2阶段弹体的减加速度变化剧烈,而弹体端部完全进入靶体后至发生贯穿阶段,弹体的减加速度变化相对较小。将计算结果与前人实验做了对比,验证了结果的可信性。 更多还原 相似文献
15.
We present a Hopkinson bar technique to evaluate the performance of accelerometers that measure large amplitude pulses, such
as those experienced during projectile penetration tests. An aluminum striker bar impacts a thin Plexiglas or copper disk
placed on the impact surface of an aluminum incident bar. The Plexiglas or copper disk pulse shaper produces a nondispersive
stress wave that propagates in the aluminum incident bar and eventually interacts with a tungsten disk at the end of the bar.
A quartz stress gage is placed between the aluminum bar and tungsten disk, and an accelerometer is mounted to the free end
of the tungsten disk. An analytical model shows that the rise time of the incident stress pulse in the aluminum bar is long
enough and the tungsten disk length is short enough that the response of the tungsten disk can be accurately approximated
as rigid-body motion. We measure stress at the aluminum bar-tungsten disk interface with the quartz gage and we calculate
rigid-body acceleration of the tungsten disk from Newton's Second Law and the stress gage data. In addition, we measure strain-time
at two locations on the aluminum incident bar to show that the incident strain pulse is nondispersive and we calculate rigid-body
acceleration of the tungsten disk from a model that uses this strain-time data. Thus, we can compare accelerations measured
with the accelerometer and accelerations calculated with models that use stress gage and strain gage measurements. We show
that all three acceleration-time pulses are in very close agreement for acceleration amplitudes to about 20,000 G. 相似文献
16.
17.
18.
Based on the acceleration data measured by penetration experiments with ogive-nose projectiles into semi-infinite concrete targets, a fuzzy method which can calculate the real-time penetration depth was developed. In the proposed method, the whole process of penetration was divided into three stages according to the instantaneous velocity, and each stage was described by different models. By judging the calculation error, threshold velocities between stages were automatically determined. Meanwhile, the striking velocity of the penetration process was calculated using the acceleration in whole trajectory. The calculated values by model are in reasonably good agreement with the measured data from experiments. 相似文献