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Normal Reflection of Shock Waves from Moving Boundaries

机译:来自运动边界的冲击波的正反射

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The problem of the reflection of a shock wave from a moving boundary is examined in an idealized one‐dimensional treatment. We consider in detail the head‐on collision of an incident step shock wave and a piston moving at constant velocity into a gas at rest. The calculation involves the head‐on collision of two shock waves and the subsequent reflection of an altered transmitted wave from the piston. The reflected pressure is calculated for a range of incident shock strengths and piston speeds. For a stationary piston both the absolute and excess reflected pressures are at most eight times the absolute or excess pressure of the incident shock wave (with γ=7/5). With a moving piston, however, this limiting factor is greater than eight, but finite for finite piston speed and infinite incident shock strength, and is infinite for infinite piston speed and finite incident shock strength. This last result holds even in the limit of the incident wave being an acoustic pulse. The method of solution for shock‐wave interaction with a piston receding at constant velocity is also indicated. Although the shock is strengthened on passing through the piston rarefaction wave, the reflected overpressure is less than that resulting from the same initial shock wave reflecting from a stationary piston.
机译:在理想的一维处理中研究了冲击波从运动边界反射的问题。我们详细考虑了入射步进冲击波与活塞以恒定速度运动成静止气体时的正面碰撞。计算涉及两个冲击波的正面碰撞,以及随后从活塞反射的透射波的反射。针对入射冲击强度和活塞速度的一系列范围计算反射压力。对于固定活塞,绝对反射压力和过量反射压力都最多为入射冲击波的绝对压力或过量压力的八倍(γ= 7/5)。然而,对于运动的活塞,该限制因子大于八,但对于有限的活塞速度和无限的入射冲击强度来说是有限的,而对于无限的活塞速度和有限的入射冲击强度来说是无限的。即使在作为声脉冲的入射波的极限内,该最后的结果也成立。还指出了与活塞以恒定速度后退的冲击波相互作用的解决方法。尽管在通过活塞稀疏波时冲击会增强,但反射的超压要小于固定活塞反射的相同初始冲击波所产生的超压。

著录项

  • 来源
    《Journal of Applied Physics 》 |1954年第3期| 共5页
  • 作者单位

    Applied Physics Laboratory, The Johns Hopkins University, Silver Spring, Maryland;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);美国《生物学医学文摘》(MEDLINE);
  • 原文格式 PDF
  • 正文语种 eng
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