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Development of a small-sized ram accelerator for improving the muzzle velocity

Development of a small-sized ram accelerator for improving the muzzle velocity
提高初速的小型冲压加速器的研制
批准号:
08555239
负责人:
SASOH Akihiro
金额:
$5.89万
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (A)
财政年份:
1996
资助国家:
日本
项目状态:
已结题
起止时间:
1996 至 1997

项目摘要

项目成果

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中文摘要
翻译
在本研究中,考虑有限速率化学反应,通过准一维数值模拟分析了标度效应。数值模拟结果表明,为了在热堵塞工作模式下获得更大的工作范围,小型装置是有利的。在此基础上,搭建了小型冲压加速器,并进行了运行试验。人们发现,设备越小,启动起来就越困难。为了更好地理解启动过程,进行了流动可视化实验。利用高速图像转换摄像机对先兆激波的行为进行了可视化。利用全息干涉术可视化了弹丸在撞锤加速管入口处撞击膜片周围的密度场,表明现有的膜片破裂模型在定量数值模拟中存在不足。通过改变混合料成分、填充压力、火药质量、弹型、破甲型和预加速段初始压力,进行了撞击加速度实验,获得了370 m/s的速度增益。
英文摘要
In this study, the scaling effects were analyzed by conducting quasi-one-dimensional numerical simulation with finite-rate chemical reactions being taken into account. From the numerical simulation, it was concluded that in order to obtain a wide operation regime in the thermally-choked operation mode, small-sized apparatus was favorable. Based on this, a small sized ram accelerator was constructed and its operation tests were conducted. It was found that the smaller the apparatus the more difficult its starting became. In order to better understand the starting process, flow visualization experiments were conducted. The behavior of a precursory shock wave was visualized by using a high-speed image converter camera. Density field around a projectile impinging the diaphragm at the ram acceleration tube entrance was visualized by holographic interferometry, concluding that the existing diaphragm rupture model was inadequate in quantitative numerical simulation. By varying mixture components, fill pressure, powder mass, projectile configuration, sabot configuration and the initial pressure in the pre-acceleration section, ram acceleration experiments were done, obtaining a velocity gain of 370 m/s.
期刊论文(19)
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会议论文
DOI: --
发表时间:
期刊:
影响因子: --
作者: []
通讯作者:
Sasoh A., Maemura J., Hirakata S., Takayama K.and Falcovitz J.: "Gasdynamics of diaphragm rupture. Impingement by a conically-nosed, ram accelerator projectile" Shock Waves. (submitted). (1998)
Sasoh A.、Maemura J.、Hirakata S.、Takayama K. 和 Falcovitz J.:“隔膜破裂的气体动力学。锥头冲压加速器射弹的撞击”冲击波。
DOI: --
发表时间:
期刊:
影响因子: --
作者: []
通讯作者:
Sasoh A., Maemura J., Hirakata S., Takayama K., Falcovitz J.: "Gasdynamics of diaphragm rupture.Impingement by a conically-nosed,ram accelelator projectile" Shock Waves. (発表予定). (1998)
Sasoh A.、Maemura J.、Hirakata S.、Takayama K.、Falcovitz J.:“隔膜破裂的气体动力学。圆锥头冲压加速器射弹的冲击”(即将发表)。
DOI: --
发表时间:
期刊:
影响因子: --
作者: []
通讯作者:
Sasoh A., Maemura J., Hirakata S., Takayama K., Falcovitz J.: "Gasdymics of aiaphragm rupture.Impingement by a conically-nosed,ram accelerator projectile" Shock Waves. (発表予定). (1998)
Sasoh A.、Maemura J.、Hirakata S.、Takayama K.、Falcovitz J.:“气动力学的隔膜破裂。锥形头冲压加速器射弹的撞击”冲击波(1998 年)。
DOI: --
发表时间:
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作者: []
通讯作者:
共 18 条
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    • 批准号:
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    • 项目类别:
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    • 资助金额:
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    Turbulence modulation simulation of sonic boom using field explosion experiments
    • 批准号:
      26630442
    • 项目类别:
      Grant-in-Aid for Challenging Exploratory Research
    • 资助金额:
      $2.5万
    • 财政年份:
      2014
    • 负责人:
      SASOH Akihiro
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    Development of actively-controlled counter driver shock tube capable of precise flow control
    • 批准号:
      25630390
    • 项目类别:
      Grant-in-Aid for Challenging Exploratory Research
    • 资助金额:
      $2.5万
    • 财政年份:
      2013
    • 负责人:
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    • 依托单位:
    Development of single-plate, two-wavelength Mach Zehnder interferometer for the measurement of unsteady density field with ionization
    • 批准号:
      24656519
    • 项目类别:
      Grant-in-Aid for Challenging Exploratory Research
    • 资助金额:
      $2.58万
    • 财政年份:
      2012
    • 负责人:
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