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高压阻塞喷注的湍流噪声
引用本文:马大猷,李沛滋,戴根华,王宏玉.高压阻塞喷注的湍流噪声[J].声学学报,1979,4(3):176-181.
作者姓名:马大猷  李沛滋  戴根华  王宏玉
作者单位:中国科学院声学研究所 (马大猷,李沛滋,戴根华),中国科学院声学研究所(王宏玉)
摘    要:过去曾求得驻点压力(表压)在0.01到10大气压适用的喷注噪声的压力关系。现在将实验扩展到100大气压过热水蒸汽,发现低压时的关系仍然适用,不过由于喷注气体不同,此时多一个附加项20log(M0/M),M0M分别是空气和喷注气体的分子量;喷注温度则几乎无影响。于是,在与喷注方向垂直,距离喷口1米处的A声级就成为${L_A} = 80 + 20\\log \\frac{D}{{{D_0}}} + 20\\log \\frac{{{M_0}}}{M} + 10\\log \\frac{{{{(P - {P_0})}^4}}}{{{P_0}^2{{(P - 0.5{P_0})}^2}}} + 10\\log \\left {\\frac{2}{\\pi }\\left( {{{\\tan }^{ - 1}}{x_A} - \\frac{{{x_A}}}{{1 + {x_A}^2}}} \\right)} \\right]$式中D为喷口直径(mm),D0为1mm, PP0分别为喷注驻压和环境大气绝对压力,在阻塞时xA=0.165D/D0实验证明在较大的温度和压力范围,噪声频谱无甚差别。管道内的扰动可使噪声级提高1-6dBA,对此本文作了理论分析。低压时使 用的小孔消声器在高压下仍然有效,但应注意其特有的关系.

收稿时间:1979-02-27

HIGH PRESSURE EXTENSION OF CHOKED JET TURBULENT NOISE THEORY
MAA Dah-You,LI Pei-zi,DAI Gen-hua,WANG Hong-yu.HIGH PRESSURE EXTENSION OF CHOKED JET TURBULENT NOISE THEORY[J].Acta Acustica,1979,4(3):176-181.
Authors:MAA Dah-You  LI Pei-zi  DAI Gen-hua  WANG Hong-yu
Abstract:A formula of pressure dependence for the turbulent noise of a cold air jet has been derived previously, holding for stagnation pressures (gauge) between 0.01 and 10 atmospheres. Experimental measurements are extended to a hundred atmospheres for superheated steam jets. It is found that the formula expressed in terms of pressures holds also in the wider range, and the jet material may be accounted for by an additional term 20log(M0/M), where ,M0 and M are the molecular weights of the air and the jet material, resp., and the jet temperature has little effect. As a consequence, the A-weighted sound level LA produced by a jet at 1 meter from the nozzle and 90° from the jet axis is shown to be ${L_A} = 80 + 20\\log \\frac{D}{{{D_0}}} + 20\\log \\frac{{{M_0}}}{M} + 10\\log \\frac{{{{(P - {P_0})}^4}}}{{{P_0}^2{{(P - 0.5{P_0})}^2}}} + 10\\log \\left {\\frac{2}{\\pi }\\left( {{{\\tan }^{ - 1}}{x_A} - \\frac{{{x_A}}}{{1 + {x_A}^2}}} \\right)} \\right]$ where D is the nozzle diameter in mm,D0 is 1 mm, P0 and P the ambient and jet stagnation pressures (absolute) resp., and for choked jets XA = 0.165D/,D0. It is also shown that the noise spectrum changes little with the temperature and stagnation pressure. Disturbance inside the pipe may make an addition to the noise level of 1-6 dBA, depending on the valve conditions. The micropore mufflers used, at low pressures are effective also at high pressures, with due considerations of diffusion properties.
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