脉冲爆轰发动机爆轰噪声场区域划分及其数值模拟

doi:10.3969/j.issn.1000-1093.2015.10.005

兵工学报 ›› 2015, Vol. 36 ›› Issue (10): 1855-1860.doi: 10.3969/j.issn.1000-1093.2015.10.005

脉冲爆轰发动机爆轰噪声场区域划分及其数值模拟

黄孝龙，许桂阳，翁春生，李宁

（南京理工大学瞬态物理国家重点实验室，江苏南京 210094）

收稿日期:2015-03-22 修回日期:2015-03-22 上线日期:2015-12-11
作者简介:黄孝龙(1988—)，男，博士研究生
基金资助:
国家自然科学基金项目（11472138）; 中央高校基本科研业务专项资金项目（30920130112007）; 国防预先研究基金项目（9140C300202120C30）

The Classification and Numerical Calculation of Noise Propagation outside Pulse Detonation Engine

HUANG Xiao-long， XU Gui-yang， WENG Chun-sheng， LI Ning

(National Key Laboratory of Transient Physics, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China)

Received:2015-03-22 Revised:2015-03-22 Online:2015-12-11

摘要/Abstract

摘要： 为了探究脉冲爆轰发动机（PDE）爆轰噪声的传播机理，根据爆轰噪声不同的非线性强度，将PDE爆轰噪声传播区域划分成强非线性区、弱非线性区和线性区3个部分，并分别采用不同的方法对各部分所对应的3种不同控制方程进行求解。数值模拟结果表明：爆轰噪声峰值声压级在出口处迅速衰减，随着轴向距离的增加，衰减速度逐渐放缓；在强非线性区，衰减速度最大值可达33 dB/m；在弱非线性区，最小衰减速度为1.02 dB/m. 模拟结果对PDE爆轰噪声的传播特性研究具有参考价值。

关键词: 兵器科学与技术, 脉冲爆轰发动机, 爆轰噪声, 衰减规律, 数值模拟

Abstract: The propagation of detonation noise is divided into three regions based on the nonlinear intensity to explore the mechanism of the noise propagation out of pulse detonation engine(PDE), which are strongly nonlinear region, weak nonlinear region and linear region. Three methods are used to solve the corresponding control equations. The calculated result shows that the detonation noise amplitude decays quickly at the jet. The rate of decay decreases with the increase in radial distance. The largest rate of decay is 33 dB/m in the strongly nonlinear region while the least rate of decay is 1.02 dB/m in the weak nonlinear region. The results are of great significance for studying the mechanism of detonation noise.

Key words: ordnance science and technology, pulse detonation engine, detonation noise, attenuation law, numerical simulation

中图分类号:

V231.2⁺2

黄孝龙，许桂阳，翁春生，李宁. 脉冲爆轰发动机爆轰噪声场区域划分及其数值模拟[J]. 兵工学报, 2015, 36(10): 1855-1860.

HUANG Xiao-long， XU Gui-yang， WENG Chun-sheng， LI Ning. The Classification and Numerical Calculation of Noise Propagation outside Pulse Detonation Engine[J]. Acta Armamentarii, 2015, 36(10): 1855-1860.

参考文献

［1］ Boesch H E, Reiff C G, Benwell B T.Modification of the acoustic spectrum of detonation tube shock waves by timed multiple-pulse addition，ARL-TR-2203［R］. America: Army Research Laboratory Report，2000.
［2］ Glaser A J, Caldwell N, Gutmark E.A fundamental study on the acoustic behavior of pulse detonation engines［C］∥45th AIAA Aerospace Sciences Meeting and Exhibit.Reno,Nevada,US: AIAA,2007.
［3］ He X, Karagozian A R . Performance and noise characteristics of pulse detonation engines［C］∥42nd AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada,US:AIAA,2004.
［4］ Eerden F V, Védy E.Propagation of shock waves from source to receiver［J］.Noise Control Engineering, 2005, 53(3):87-93.
［5］王秉义.枪炮噪声与爆炸声的特性和防治［M］. 北京：国防工业出版社, 2001:31-32．
WANG Bing-yi.Gun muzzle noise & explosive sound-Character,Protection and control［M］. Beijing： National Defence Industry Press, 2001:31-32．（in Chinese）
［6］王杰, 翁春生.脉冲爆轰发动机冲击波外流场数值模拟［J］.火炮发射与控制学报, 2009, 30(3):53-56.
WANG Jie,WENG Chun-sheng. Numerical simulation shock wave exteral flow of pulse detonation engine［J］. Journal of Gun Launch & Control, 2009，30(3):53-56.（in Chinese）
［7］王研艳, 翁春生.尾喷管构型对多循环两相脉冲爆轰发动机流场及性能影响［J］.航空动力学报, 2013, 28(10):66-69.
WANG Yan-yan, WENG Chun-sheng. Effects of nozzle on flow field and performance of multi-cycle two-phase pulse detonation engines［J］. Journal of Aerospace Power， 2013,28(10): 66-69. （in Chinese）
［8］ Chang S C.The method of space-time conser vation element and solution element-a new approach for solving the navier-stokes and euler equations［J］. Journal of Computational Physics,1995,119(2): 295-324.
［9］ Piacsek A A, Locey L L, Sparrow V W. Time-domain modeling of atmospheric turbulence effects on sonic boom propagation［C］ ∥14th AIAA/CEAS Aeroacoustics Conference. Vancouver, British Columbia, Canada: AIAA,2008.
［10］ Piacsek A A, Plotkin K J. Application of nonlinear progressive-wave equation to sonic boom transition focus［C］ ∥51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Grapevine, Texas, US:AIAA,2013.

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脉冲爆轰发动机爆轰噪声场区域划分及其数值模拟

The Classification and Numerical Calculation of Noise Propagation outside Pulse Detonation Engine

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