期刊文献+

潜艇水下武器发射后海水喷流噪声数值仿真 被引量:3

Simulation on Seawater Jet Noise after Submarine Underwater Launching
下载PDF
导出
摘要 为了研究武器发射出管后的海水喷流噪声,将发射管比拟为水下圆管,通过发射装置水下发射过程的3D流场仿真,获取了武器出管后发射管口海水喷流的流场特性,在此基础上采用基于Lighthill声学类比的积分方法对水下圆管自由喷流噪声进行了计算与分析。结果表明,喷流噪声的能量主要集中在100 Hz以下的低频范围内,水下武器发射后的海水喷流噪声源并不是总发射噪声的主要组成。 To study the noise of the seawater jet from a submarine launch tube after a weapon leaving the tube, simula- tion on three-dimensional flow field of the launching process is conducted, and the fluid field of the seawater jet at noz- zle after the weapon leaving the tube is obtained. The free jet noise of underwater round pipe is calculated using the Lighthill acoustic analogy integral method based on the seawater jet fluid characteristic. Calculation result shows that the energy of seawater jet noise concentrates in the low frequency noise (lower than 100 Hz), and the seawater jet noise is not the main component of the overall launching noise.
出处 《鱼雷技术》 2015年第1期61-65,共5页 Torpedo Technology
关键词 潜艇水下发射 海水喷流 噪声 仿真 submarine underwater launching seawater jet noise simulation
  • 相关文献

参考文献6

  • 1练永庆,王树宗.武器发射装置设计原理[M].北京:国防工业出版社,2012:65-66.
  • 2Issa R I. Solution of Implicitly Discredited Fluid Flow Equations by Operator Splitting[J]. Journal of Computa- tional Physics, 1986(62): 40-65.
  • 3Tam C K W. Jet Noise: Since 1952[J]. Theoretical and Computational Fluid Dynamics. 1998, 10(1): 393-405.
  • 4李晓东,江旻,高军辉,林大楷,刘黎,李小艳.计算气动声学进展与展望[J].中国科学:物理学、力学、天文学,2014,44(3):234-248. 被引量:17
  • 5Ffowcs W J E, Kempton A J. The Noise from the Large- scale Structure of a Jet[J]. Journal of Fluid Mechanics, 1978, 84(4): 673-694.
  • 6郭新毅,马力.环境变化条件下海洋环境噪声统计分析[C]//2010中国西部地区声学学术交流会.云南:中国声学学会,2010:338-341.

二级参考文献87

  • 1Lighthill M J. On sound generated aerodynamically: Ⅰ. General theory. Proc R Soc Lond A, 1952, 211: 564-581.
  • 2Lighthill M J. On sound generated aerodynamically: Ⅱ. Turbulence as a source of sound. Proc R Soc Lond A, 1954, 211: 1-31.
  • 3Ffowcs Williams J E, Hawkings D L. Sound generated by turbulence and surfaces in arbitrary motion. Phil Trans R Soc Lond A, 1969, 264(1151): 321-342.
  • 4Tam C K W. Computational aeroacoustics: An overview of computational challenges and applications. Int J Comput Fluid Dyn, 2004, 18(6): 547-567.
  • 5Tam C K W. Computational aeroacoustics: Issues and method. AIAA J, 1995, 33(10): 1788-1796.
  • 6Tam C K W. Advances in numerical boundary conditions for computational aeroacoustics. J Comput Acoust, 1998, 6(4): 377-402.
  • 7Tam C K W. Computational Aeroacoustics, A Wave Number Approach. London: Cambridge University Press, 2012.
  • 8Lele S K. Computational aeroacoustics: A review. In: the Proceedings of 35th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reno: American Institute of Aeronautics and Astronautics, 1997. 0018.
  • 9Lele S K. Compact finite difference scheme with spectral-like resolution. J Comput Phys, 1992, 103(1): 16-42.
  • 10Tam C K W, Webb J C. Dispersion-relation-preserving finite difference scheme for computational acoustics. J Comput Phys, 1993, 107(2): 262-281.

共引文献16

同被引文献24

  • 1杨琼方.潜艇流噪声和推进器噪声的数值预报和分析[D].武汉:海军工程大学船舶与动力学院,2011.
  • 2McDufford M D.Identification of noise sources in a heated jet flow[D].Columbus:Department of Mechanical Engineering,The Ohio State University,2006.
  • 3Hileman J.Large-scale structures and noise generation in high-speed jets[D].Columbus:Department of Mechanical Engineering,The Ohio State University,2004.
  • 4Caridi D.Industrial CFD simulation of aerodynamic noise[D].Napoli:Dipartimento di Ingegneria Aerospaziale,Universitàdegli studi di Napoli Federico II,2008.
  • 5ANSYS.ANSYS Fluent 14.0user's guide[R].Pittsburgh:ANSYSInc,2011.
  • 6Robinson D.Acoustics modeling in CFX[J].The Focus,2007,60(9):3-5.
  • 7Wang M,Freund J B,Lele S K.Computation prediction of flow-generated sound[J].Annual Review of Fluid Mechanics,2006,38:483-512.
  • 8Kato C,Yamade Y,Wang H,et al.Numerical prediction of sound generated from flows with a low Mach number[J].Computers&Fluids,2007,36:53-68.
  • 9Lyrintzis A S.Surface integral methods in computational aeroacoutics-from the(CFD)near-field to the(Acoustic)far-field[J].International Journal of Aeroacoustics,2003,2(2):95-128.
  • 10喻荣兵,陈建勇,谢志敏.负跃层对主动声纳探测距离影响仿真研究[J].海军航空工程学院学报,2009,24(2):141-143. 被引量:3

引证文献3

二级引证文献9

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部