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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,通过考虑有限速率化学反应的准一维数值模拟,分析了结垢效应。数值模拟结果表明,在热阻工况下,为了获得较宽的运行区域,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。结果发现,仪器越小,启动就越困难。为了更好地了解启动过程,进行了流动可视化实验。利用高速图像转换相机对前兆冲击波的行为进行了可视化。利用全息干涉法对冲压加速管入口处弹丸撞击横隔板周围的密度场进行了可视化,得出了现有横隔板破裂模型在定量数值模拟中的不足。通过改变混合气组成、充填压力、药剂质量、弹丸构型、弹托构型和预加速度段的初始压力,进行了冲压加速实验,获得了370m/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: --
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作者: []
通讯作者:
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