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Development and analysis of a leak-based blast attenuator and scaling laws for primary blast peak overpressure for a large caliber muzzleloaded cannon.

机译:开发和分析基于泄漏的爆炸衰减器,以及针对大型口径大炮加载的原始爆炸峰值超压的定律。

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摘要

One of the primary aspects of the research and development work carried out at Benet Laboratories is the Soldier. Maintenance of their health in the field is the first priority while the second priority is the enhancement of their performance. Therefore, a new concept for a weapon system that targets these two priorities is highly desirable. This is the case with a new concept that can reduce the peak overpressure without the use of a muzzle device for a muzzle loaded cannon system. Such a novel concept was developed in this thesis through the application of propellant leak into the precursor region, i.e., when the projectile is still in the bore. A 3D hydrocode (ALE3D) was employed to predict the blast overpressure for the baseline and propellant leak configurations. However, a 3D hydrocode is computationally very expensive to predict peak overpressure in the far-field and an efficient method to predict peak overpressure in the far-field is of significance. Therefore, scaling laws for primary blast peak overpressure were also developed in this thesis.;Initially, two propellant leak concepts were examined. A bulge leak method and a channel leak method, which were compared to the baseline configuration. The initial channel leak configuration (referred to as CLM-1) significantly reduced the exit pressure ratio during projectile ejection, and thereby, resulted in a weaker blast. This in-turn substantially attenuated the peak overpressure to the rear of the muzzle without the aid of a muzzle device while having a marginal loss in the projectile exit velocity. For CLM-1, at one monitored location with the largest peak overpressure, a reduction of about 38% in peak overpressure was observed as compared to the baseline case. In order to compare different leak configurations, a performance metric was defined by comparing the ratio of peak overpressure and projectile exit velocity for a leak configuration to that for the baseline configuration. This metric was referred to as the Figure of Merit (FoM) and defined for any probe location. An average FoM was also defined based on the average of local FoM over different locations/probes. The greater the FoM is above zero, the better the configuration. The average FoM for the CLM-1 configuration was 0.221. In addition to FoM, shock structure and strength were also analyzed for the bulge and channel configurations at both the precursor and blast stages.;With the success of the CLM-1 configuration, we then performed a parametric study of the channel leak geometry and examined the effect of different geometric parameters on peak overpressure attenuation. The idea was to further improve the performance of the channel leak method. We divided our parametric study into five groups (i.e., A through E), referred to as CLM-A through CLM-E configurations. The focus in these five groups was on geometric parameters that were expected to be the most influential or relevant. Three relevant geometric parameters were considered in this work. In groups A and B, we focused on channel leak volume. Group C analyzed the effect of channel length while groups D and E investigated the effect of aspect ratio. The five groups were ordered in this way because we anticipated the total leak volume to be the most influential parameter, then the channel length which was followed by the aspect ratio. The total leak volume of 7.5% resulted in a relatively high average FoM. On the other hand, the use of channels with a shorter length was found to be detrimental while a lower value of aspect ratio was beneficial. Three leak configurations of CLM-A1, CLM-E1 and CLM-E2 provided excellent peak overpressure attenuation (i.e., above 45% and up to 63%). Each led to an average FoM above 0.5 while CLM-E configurations resulted in lower local FoM for probes near the muzzle and higher FoM for probes farther from the muzzle, and thus, a higher variation of FoM over the probes. The average FoM based on the far-field probes was about 0.575 and 0.560 for CLM-E1 and CLM-E2, respectively, and 0.520 for CLM-A1. Blast structure and strength were also analyzed for these three configurations.;In the last part of this thesis, we focused on the baseline and CLM-A1 configurations in order to develop scaling laws for the primary blast peak overpressure. Two different power-law scaling techniques were considered. In the first power-law, scaling parameters were defined from the muzzle center. The second power-law scaling was defined based on the blast center. The muzzle center based power-law has been used in the past while the blast center based power-law is a newly developed scaling law in this thesis. For the baseline configuration, both scaling laws performed well and for many locations absolute difference was below 10%. For the CLM-A1 configuration, blast center based power-law predictions were better than those from the muzzle center based power-law and showed a better overall correlation with the ALE3D predictions.
机译:贝纳特实验室进行的研发工作的主要方面之一是士兵。在野外维护他们的健康是第一要务,而第二要务是增强其性能。因此,迫切需要针对这两个优先事项的武器系统的新概念。新概念就是这种情况,可以在不将枪口装置用于装有枪口的加农炮系统的情况下降低峰值超压。通过将推进剂泄漏施加到前体区域中,即当射弹仍在孔中时,在本文中提出了这样的新颖概念。使用3D液压代码(ALE3D)来预测基线和推进剂泄漏配置的爆炸超压。但是,3D液压代码在预测远场中的峰值超压方面在计算上非常昂贵,而预测远场中的峰值超压的有效方法很重要。因此,本文还建立了爆炸峰值超压的定标规律。最初,研究了两种推进剂泄漏的概念。将膨胀泄漏方法和通道泄漏方法与基线配置进行了比较。初始通道泄漏配置(称为CLM-1)显着降低了弹丸弹射过程中的出口压力比,从而导致了较弱的爆炸。依次地,这在没有炮弹装置的情况下大大减弱了到炮口后部的峰值过压,同时在弹丸出口速度上有一点损失。对于CLM-1,在一个监测到的峰值超压最大的位置,与基线情况相比,峰值超压降低了约38%。为了比较不同的泄漏配置,通过比较泄漏配置的峰值过压和弹丸出口速度与基准配置的峰值超压和弹丸出口速度之比来定义性能指标。此度量标准称为品质因数(FoM),并针对任何探针位置进行了定义。还基于不同位置/探针上本地FoM的平均值来定义平均FoM。 FoM大于零越大,配置越好。 CLM-1配置的平均FoM为0.221。除了FoM之外,还分析了前兆和爆炸阶段的凸起和通道构型的冲击结构和强度。随着CLM-1构型的成功,我们随后对通道泄漏的几何形状进行了参数研究并检查了不同几何参数对峰值超压衰减的影响。想法是进一步提高通道泄漏方法的性能。我们将参数研究分为五个组(即A到E),称为CLM-A到CLM-E配置。这五个组的重点是预期最有影响力或最相关的几何参数。在这项工作中考虑了三个相关的几何参数。在A组和B组中,我们集中于通道泄漏量。 C组分析了通道长度的影响,而D组和E组则研究了纵横比的影响。以这种方式对这五个组进行排序是因为我们预计总泄漏量是最有影响力的参数,然后是通道长度,然后是长宽比。总泄漏量为7.5%,导致平均FoM较高。另一方面,发现使用较短长度的通道是有害的,而较低的纵横比值是有益的。 CLM-A1,CLM-E1和CLM-E2的三种泄漏配置提供了出色的峰值过压衰减(即,高于45%且高达63%)。每个导致平均FoM高于0.5,而CLM-E配置导致靠近枪口的探针的局部FoM较低,而远离枪口的探针的FoM较高,因此,整个探针的FoM变化较大。基于远场探针的平均FoM对CLM-E1和CLM-E2分别约为0.575和0.560,对CLM-A1为0.520。还对这三种构造的爆破结构和强度进行了分析。本论文的最后一部分,我们集中在基线和CLM-A1构造上,以便为主要爆破峰超压制定定律。考虑了两种不同的幂律定标技术。在第一个幂律中,缩放参数是从枪口中心定义的。根据爆炸中心定义了第二幂律定标。过去使用基于枪口中心的功率定律,而基于爆炸中心的功率定律是本文中新开发的缩放定律。对于基准配置,两种缩放定律均表现良好,并且在许多位置,绝对差均低于10%。对于CLM-A1配置,基于爆炸中心的功率定律预测优于基于炮口中心的功率定律,并且与ALE3D预测具有更好的整体相关性。

著录项

  • 作者

    Carson, Robert Andrew.;

  • 作者单位

    Rensselaer Polytechnic Institute.;

  • 授予单位 Rensselaer Polytechnic Institute.;
  • 学科 Aerospace engineering.
  • 学位 Ph.D.
  • 年度 2014
  • 页码 157 p.
  • 总页数 157
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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