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封闭状态储运发射箱箱壁压力的子波分析

Wavelet analysis of exhausted flow field pressure in closed container-launcher

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【作者】 徐强张福祥廖光煊范维澄

【Author】 XU Qiang 1, ZHANG Fu-xiang 2, LIAO Guang-xuan 1, FAN Wei-cheng 1 (1.State Key Lab. of Fire Science, University of Sci. & Tech. of China, Hefei 230026, China; 2. Dept. of Mech., Nanjing University of Sci.& Tech., Nanjing 210094, China)

【机构】 中国科学技术大学火灾科学国家重点实验室南京理工大学机械学院中国科学技术大学火灾科学国家重点实验室 安徽合肥230026江苏南京210014安徽合肥230026安徽合肥230026

【摘要】 为研究火箭导弹在封闭式储运发射箱内发射时 ,由于密封盖的反射作用使弹箱间隙内存在的复杂燃气流场 ,通过对测量数据进行子波分析 ,得到了管 (箱 )壁压力时间历程曲线中的燃气射流段是由射流激波振荡 (低频 )和射流噪声 (高频 )两种流动成分组合而成 ,激波振荡沿管壁向弹头方向是衰减的 ,它在低频段聚积的能量与起始冲击波一起都对储运发射箱式定向器具有破坏作用。

【Abstract】 A set of experimental studies were conducted to study complicated internal exhausted flow field generated by missile which was launched from a closed container-launcher.Wavelet transform method was used to analyze the wall pressure-time history data,and shock wave oscillation(low frequency)and jet noise (high frequency) were found in the exhausted flow section.Shock wave oscillation is attenuated along launcher wall at the direction to missile head.Its energy focuses on low frequency band and it is harmful to container-launcher along with initial shock wave.

  • 【文献出处】 流体力学实验与测量 ,Experiments and Measurements In Fluid Mechanics , 编辑部邮箱 ,2001年03期
  • 【分类号】O354.5
  • 【被引频次】1
  • 【下载频次】81
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