西北工业大学 翼型叶栅空气动力学重点实验室,西安,710072
刘秋洪*(1977-),男,湖南株洲人,博士,副教授,研究方向:空气动力学、气动声学. E-mail: qhliu@nwpu.edu.cn
纸质出版:2023
移动端阅览
刘秋洪, 王垿桁, 薛丝丹, 等. 均匀流中声学速度预测的时域解析公式[J]. 空气动力学学报, 2023, 41(7): 84−92.
LIU Qiuhong, WANG Xuheng, XUE Sidan, et al. Time-domain analytical formulation for acoustic velocity prediction in uniform mean flow[J]. 2023, 41(7): 84-92.
刘秋洪, 王垿桁, 薛丝丹, 等. 均匀流中声学速度预测的时域解析公式[J]. 空气动力学学报, 2023, 41(7): 84−92. DOI: 10.7638/kqdlxxb-2022.0073
LIU Qiuhong, WANG Xuheng, XUE Sidan, et al. Time-domain analytical formulation for acoustic velocity prediction in uniform mean flow[J]. 2023, 41(7): 84-92. DOI: 10.7638/kqdlxxb-2022.0073.
采用理论解析和数值计算方法研究均匀流中声学速度预测的时域解析公式。对基于可渗透面原理的声学速度预测,理论分析了对流矢量波动方程的右端源项,结果显示部分对声学速度传播有贡献的可渗透面源被忽略。基于对流矢量波动方程时域积分公式V1A-M,进一步考虑丢失可渗透面源的贡献,发展了解析公式CV1A-M。对均匀平均流中静止与旋转的单极子和偶极子,利用公式V1A-M和CV1A-M数值预测了点源辐射的声学速度。公式CV1A-M数值解与理论值吻合一致,公式V1A-M因可渗透面载荷源部分丢失,数值解与理论值差异明显。均匀流中偶极子点源声辐射不会诱发涡波扰动,线化欧拉方程能够描述声学速度与声学压力间关系。
The time-domain analytical formulation for acoustic velocity prediction in a uniform mean flow is considered theoretically and numerically. For acoustic velocity prediction based on the permeable surface principle
a theoretical analysis of the source terms on the right hand of the convective vector wave equation shows that part of the permeable surface source contributing to the acoustic velocity propagation is neglected. Based on the time-domain integral formulation V1A-M for the convective vector wave equation
an analytical formulation CV1A-M is developed by further considering the contribution from the missing permeable surface source. The acoustic velocity radiations are predicted numerically using formulations V1A-M and CV1A-M for a stationary/rotating monopole and dipole in a uniform mean flow. The numerical solutions of formulation CV1A-M agree well with the theoretical values
while the numerical solutions of formulation V1A-M differ significantly from the theoretical values due to the neglection of part of the loading source on the permeable surface. The radiation from a dipole in a uniform mean flow dose not induce any vortical disturbance and the linearised Euler equation can be used to describe the relationship between acoustic velocity and acoustic pressure.
FFOWCS WILLIANMS J E, HAWKINGS D L. Sound generation by turbulence and surfaces in arbitrary motion[J]. Philosophical Transactions of the Royal Society A: Mathematical and Physical Sciences, 1969, 264(1151): 321-342. DOI:10.1098/rsta.1969.0031
NAJAFI-YAZDI A, BRÈS G A, MONGEAU L. An acoustic analogy formulation for moving sources in uniformly moving media[J]. Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, 2011, 467(2125): 144-165. DOI:10.1098/rspa.2010.0172[LinkOut]
GHORBANIASL G, LACOR C. A moving medium formulation for prediction of propeller noise at incidence[J]. Journal of Sound and Vibration, 2012, 331(1): 117-137. DOI:10.1016/j.jsv.2011.08.018[LinkOut]
ZHONG S Y, ZHANG X. A sound extrapolation method for aeroacoustics far-field prediction in presence of vortical waves[J]. Journal of Fluid Mechanics, 2017, 820: 424-450. DOI:10.1017/jfm.2017.219[LinkOut]
FARASSAT F. Derivation of formulations 1 and 1A of farassat[R]. NASA/TM-2007-214853, 2007
DUNN M H. The acoustic analogy in four dimensions[J]. International Journal of Aeroacoustics, 2019, 18(8): 711-751. DOI:10.1177/1475472X19890259
MAO Y J, XU C, QI D T. Computation of instantaneous and time-averaged active acoustic intensity field around rotating source[J]. Journal of Sound and Vibration, 2015, 337: 95-115. DOI:10.1016/j.jsv.2014.10.023[LinkOut]
CROAKER P, KESSISSOGLOU N, MARBURG S. Aeroacoustic scattering using a particle accelerated computational fluid dynamics/boundary element technique[J]. AIAA Journal, 2016, 54(7): 2116-2133. DOI:10.2514/1.J054260[LinkOut]
XU C, MAO Y J, HU Z W. Improved equivalent source method to predict sound scattered by solid surfaces[J]. AIAA Journal, 2018, 57(2): 513-520. DOI:10.2514/1.J057490[LinkOut]
LEE S, BRENTNER K S, MORRIS P J. Assessment of time-domain equivalent source method for acoustic scattering[J]. AIAA Journal, 2011, 49(9): 1897-1906. DOI:10.2514/1.J050736[LinkOut]
MAO Y J, CAI J C, GU Y Y, et al. Direct evaluation of acoustic-intensity vector field around an impedance scattering body[J]. AIAA Journal, 2014, 53(5): 1362-1371. DOI:10.2514/1.J053431[LinkOut]
FARASSAT F, BRENTNER K. The derivation of the gradient of the acoustic pressure on a moving surface for application to the fast scattering code (FSC)[R]. NASA/TM-2005-213777, 2005.
LEE S, BRENTNER K S, FARASSAT F, et al. Analytic formulation and numerical implementation of an acoustic pressure gradient prediction[J]. Journal of Sound and Vibration, 2009, 319(3-5): 1200-1221. DOI:10.1016/j.jsv.2008.06.028[LinkOut]
LEE S, BRENTNER K S, MORRIS P J. Time-domain approach for acoustic scattering of rotorcraft noise[J]. Journal of the American Helicopter Society, 2012, 57(4): 1-12. DOI:10.4050/jahs.57.042001[LinkOut]
GHORBANIASL G, HUANG Z J, SIOZOS-ROUSOULIS L, et al. Analytical acoustic pressure gradient prediction for moving medium problems[J]. Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, 2015, 471(2184): 20150342. DOI:10.1098/rspa.2015.0342[LinkOut]
BI C X, WANG Z H, ZHANG X Z. Analytic time-domain formulation for acoustic pressure gradient prediction in a moving medium[J]. AIAA Journal, 2017, 55(8): 2607-2616. DOI:10.2514/1.J055630[LinkOut]
GHORBANIASL G, CARLEY M, LACOR C. Acoustic velocity formulation for sources in arbitrary motion[J]. AIAA Journal, 2012, 51(3): 632-642. DOI:10.2514/1.J051958[LinkOut]
MAO Y J, ZHANG Q L, XU C, et al. Two types of frequency-domain acoustic-velocity formulations for rotating thickness and loading sources[J]. AIAA Journal, 2014, 53(3): 713-722. DOI:10.2514/1.J053230[LinkOut]
MAO Y J, GU Y Y, XU C. Validation of frequency-domain method to compute noise radiated from rotating source and scattered by surface[J]. AIAA Journal, 2016, 54(4): 1188-1197. DOI:10.2514/1.J053674[LinkOut]
LEE S, BRENTNER K S. Comment on “acoustic velocity formulation for sources in arbitrary motion”[J]. AIAA Journal, 2016, 54(5): 1810-1811. DOI:10.2514/1.J054845[LinkOut]
MAO Y J, TANG H T, XU C. Vector wave equation of aeroacoustics and acoustic velocity formulations for quadrupole source[J]. AIAA Journal, 2016, 54(6): 1922-1931. DOI:10.2514/1.J054687[LinkOut]
KAMBE T. A new formulation of equations of compressible fluids by analogy with Maxwell's equations[J]. Fluid Dynamics Research, 2010, 42(5): 055502. DOI:10.1088/0169-5983/42/5/055502[LinkOut]
MAO Y J, HU Z W, XU C, et al. Vector aeroacoustics for uniform mean flow: acoustic velocity and vortical velocity[J]. AIAA Journal, 2018, 56(7): 2782-2793. DOI:10.2514/1.J056852[LinkOut]
CASALINO D. An advanced time approach for acoustic analogy predictions[J]. Journal of Sound and Vibration, 2003, 261(4): 583-612. DOI:10.1016/S0022-460X(02)00986-0[LinkOut]
0
浏览量
0
下载量
0
CSCD
关联资源
相关文章
相关作者
相关机构
京公网安备11010802024621