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Measurement and analysis of noise field of rocket engine based on statistical energy analysis(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2010年03期
Page:
49-53
Research Field:
测控与试验
Publishing date:

Info

Title:
Measurement and analysis of noise field of rocket engine based on statistical energy analysis
Author(s):
Liu Xiaoyong Li Jun Zhou Yunduan
Xi'an Aerospace Propulsion Institute, Xi'an 710100, China
Keywords:
-
PACS:
V434
DOI:
-
Abstract:
The jet noise and specific sound field produced by a rocket engine on the ground test stand were measured, and the vibro-acoustic model was built based on statistical energy analysis to predict the noise environment of the rocket engine. During the test, the sound pressure levels around the engine nozzle and the payload cabin were measured. The result can support the noise spectrum prediction of the key rocket part.

References:

[1]宋文治. NASA在声振领域研究的新成果[J]. 强度与环境. 2006, 33(2): 58-64. [2]冯涛, 王晶. 声学中的数值模拟方法及其应用范围[J]. 北京工商大学学报. 2004, 22(1): 41-43. [3]商德江. 加肋双层圆柱壳振动声辐射数值计算分析[J]. 声学学报, 2001, 26(3): 193-201. [4]王其政. 结构藕合动力学[M]. 北京: 宇航出版社, 1999. [5]Bharj T, Cimerman B. Application of Statistical Energy Analysis to a Passenger Vehicle: Combining Analytical and Test-Based Prediction in a Hybrid Model[C]. Proceeding of Inter Noise, 1996, Liverpool: 1303-1306. [6]Parrett A V, Hicks B, John K. Statistical Energy Analysis of Airborne and Structure-Borne Automobile[C]. Proceed-ings of Inter Noise, 1997. [7]盛美萍. 复杂耦合系统的统计能量分析及其应用[J]. 中国工程科学, 2002, 4(6): 77-84. [8]聂旭涛, 熊飞峤. 运用统计能量分析法预示空空导弹舱内动力学环境[J]. 振动与冲击, 2007, 26(4): 140-143. [9]胡莹, 陈克安, 潘凯. 基于统计能量分析的飞机舱室降噪研究[J]. 噪声与振动控制. 2007, 04(2): 65-68. [10]刘小勇, 盛美萍, 雷烨, 等. 双层圆柱壳噪声预报及统计能量参数灵敏度分析[J]. 振动与冲击. 2007, 26(7): 50-53. [11]谢久林, 杨松, 张俊刚, 等. 航天器声振动力学环境响应分析[J]. 航天器环境工程, 2006, 23(2): 83-86. [12]姚德源, 王其政. 统计能量分析原理及其应用[M]. 北京: 北京理工大学出版社, 1995. [13]仲伟聪, 张锋. 单喷嘴燃烧流场仿真研究[J]. 火箭推进, 2009, 35(6): 27-30. [14]李琪琪, 叶斌, 陈锋, 等. 液体火箭发动机试验频率量信号的处理与仿真[J]. 火箭推进, 2008, 34(5): 39-42.

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