[1]王良锋, 乔渭阳, 纪良,等.风扇进口噪声预测模型的改进[J].推进技术,2015,36(2): 226-231.
WANG Liangfeng, QIAO Weiyang, JI Liang, et al. An improved prediction model for fan inlet noise[J]. Journal of Propulsion Technology, 2015,36(2): 226-231.
[2]WOODWARD R, HUGHES C, JERACKI R, et al. Fan noise source diagnostic test: far-field acoustic results[C]//8th AIAA/CEAS Aeroacoustics Conference & Exhibit. Breckenridge: AIAA, 2002.
[3]NALLASAMY M, ENVIA E. Computation of rotor wake turbulence noise[J]. Journal of Sound & Vibration, 2005,282(3): 649-678.
[4]MORIN B L. Broadband fan noise prediction system for turbofan engines. Volume 3: BFANS validation and test cases: CR-2010-216898[R]. Washington, D.C.: NASA, 2010.
[5]POSSON H, MOREAU S, ROGER M. Broadband noise prediction of fan outlet guide vane using a cascade response function[J]. Journal of Sound & Vibration, 2011,330(25): 6153-6183.
[6]FFOWCS WILLIAMS J E, HAWKINGS D L. Sound generation by turbulence and surfaces in arbitrary motion[J]. Philosophical Transcations of the Royal Society A, 1969,264(1151): 321-342.
[7]张建华, 楚武利, 刘炜.单级轴流风扇单音噪声源及噪声辐射特性的数值研究[J]. 动力工程学报, 2015,35(7): 574-580.
ZHANG Jianhua, CHU Wuli, LIU Wei. Numerical study on tone noise source and noise radiation characteristics of single stage axial flow fan[J]. Journal of Chinese Society of Power Engineering, 2015,35(7): 574-580.
[8]SEARS W R. Some aspects of non-stationary airfoil theory and its practical application[J]. Journal of Aeronautical Sciences, 1941,8(3): 104-108.
[9]WHITEHEAD D, MECH E M I. Vibration and sound generation in a cascade of flat plates in subsonic flow: CUED/A-Turbo/TR15[R]. Cambridge: Cambridge University Engineering Laboratory, 1972.
[10]SMITH S N. Discrete frequency sound generation in axial flow turbomachines[R]. [S.l.]: Aeronautical Research Council Reports and Memoranda, 1973.
[11]NAMBA M. Three-dimensional analysis of blade force and sound generation for an annular cascade in distorted flows[J]. Journal of Sound & Vibration, 1977,50(4): 479-508.
[12]乔渭阳. 桨扇近场噪声的FFT算法[J]. 航空学报, 1993,14(6): 254-262.
QIAO Weiyang. A numerical prediction method for the near-field harmonic noise of prop-fan[J]. Acta Aeronautica et Astronautica Sinica, 1993,14(6): 254-262.
[13]ZHANG W, WANG X, SUN X. A broadband noise model for turbulence/annular-cascade interaction[C]//AIAA/CEAS Aeroacoustics Conference. Berlin: AIAA,2013.
[14]ZHANG W G, WANG X Y, SUN X F. Predictions of fan broadband noise using lifting surface method[J]. AIAA Journal, 2015,53(10): 1-11
[15]左曙光, 何慧娟, 吴旭东, 等.叶片旋转噪声激励下漩涡风机壳体声辐射计算理论及分析[J]. 振动与冲击, 2015,34(24): 59-65.
ZUO Shuguang, HE Huijuan, WU Xudong, et al. Study of the regenerative blower’s shell sound radiation under the rotational noise excitation [J]. Journal of Vibration and Shock, 2015,34(24): 59-65.
[16]李晓东,段传波,于潮. 三维FW-H方程与CAA数值模拟匹配技术研究[J].工程热物理学报, 2005,26(1): 51-54.
LI Xiaodong, DUAN Chuanbo, YU Chao. On the matching technology between the 3D FW-H equation and CAA numerical simulations[J]. Journal of Engineering Thermophysics, 2005,26(1): 51-54.
[17]MANI R, HORVAY G. Sound transmission through blade[J]. Journal of Sound & Vibration, 1970,12(1): 59-83.
[18]KOCH W. On the transmission of sound waves through a blade row[J]. Journal of Sound & Vibration, 1971,18(1): 111-128.
[19]PEAKE N. The interaction between a high-frequency gust and a blade row[J]. Journal of Fluid Mechanics, 1992,241(1): 261-289.
[20]PEAKE N. The scattering of vorticity waves by an infinite cascade of flat plates in subsonic flow[J]. Wave Motion, 1993,18(3): 255-271.
[21]GLEGG S A L. The response of a swept blade row to a three-dimensional gust[J]. Journal of Sound & Vibration, 1999,227(1): 29-64.
[22]POSSON H, ROGER M, MOREAU S. On a uniformly valid analytical rectilinear cascade response function[J]. Journal of Fluid Mechanics, 2010,663: 22-52.
[23]POSSON H, ROGER M. Experimental validation of a cascade response function for fan broadband noise predictions[J]. AIAA Journal, 2012,49(9): 1907-1918.
[24]HANSON D B.Theory of broadband noise for rotor and stator cascade with inhomogeneous inflow turbulence including effects of lean and sweep: CR-210762[R]. Washington, D.C.: NASA, 2001.
[25]HANSON D B. Predicting broadband noise from a stator vane of a gas turbine engine: US 6353789 B1[P]. 2002-03-05.
[26]GANZ U, JOPPA P, PATTEN T, et al. Boeing 18-inch fan rig broadband noise test: CR-1998-208704[R]. Washington, D.C.: NASA, 1998.
[27]STEWART A L. Broadband fan noise generated by small scale turbulence: CR-207752[R]. Washington, D.C.: NASA, 1998.
|