直升机旋翼气动噪声的研究新进展

doi:10.7527/S1000-6893.2017.520991

直升机技术专栏

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直升机旋翼气动噪声的研究新进展

徐国华¹, 史勇杰¹, 招启军¹, 王阳², 樊枫³

1. 南京航空航天大学直升机旋翼动力学国家级重点实验室, 南京 210016;
2. 南京航空航天大学无人机研究院, 南京 210016;
3. 中国直升机设计研究所, 景德镇 333000

收稿日期:2016-11-28 修回日期:2017-02-28 出版日期:2017-07-15 发布日期:2017-04-17
通讯作者: 徐国华,E-mail:ghxu@nuaa.edu.cn E-mail:ghxu@nuaa.edu.cn

New research progress in helicopter rotor aerodynamic noise

XU Guohua¹, SHI Yongjie¹, ZHAO Qijun¹, WANG Yang², FAN Feng³

1. National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
2. Research Institute of Unmanned Aircraft, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
3. China Helicopter Research and Development Institute, Jingdezhen 333000, China

Received:2016-11-28 Revised:2017-02-28 Online:2017-07-15 Published:2017-04-17

摘要/Abstract

摘要：

随着直升机的广泛使用，旋翼气动噪声问题逐渐得到重视。概述了旋翼厚度噪声、载荷噪声、高速脉冲（HSI）噪声、桨-涡干扰（BVI）噪声和宽带噪声的国内外研究现状，简述了旋翼气动噪声理论、试验、计算发展历程以及各阶段的研究成果，并对后缘襟翼、高阶谐波控制（HHC）、单片桨叶控制（IBC）、主动扭转桨叶等噪声控制方法和概念进行了介绍。重点叙述了旋翼气动噪声的研究新进展，包括大气、地面和飞行轨迹等对直升机旋翼噪声的影响，机身散射声场以及机动噪声计算方法等方面取得的成就。对直升机旋翼气动噪声的研究进行了总结，并对其发展前景提出了展望。

关键词: 直升机, 旋翼噪声, 桨-涡干扰噪声, 高速脉冲噪声, 降噪技术, 机身散射声场, 机动噪声

Abstract:

Helicopter rotor aerodynamic noise has become an important research topic in helicopter technology with the widespread use of helicopters. This paper outlines the current status of the research on rotor thickness noise, loading noise, high speed impulsive (HSI) noise, blade vortex interaction (BVI) noise, and broadband noise. Domestic and foreign research on numerical calculation methods and experimental methods for rotor noise are reviewed, and the application of trailing-edge flap, higher harmonic control (HHC), individual blade control (IBC) and active twist blade to rotor noise control are also introduced. The latest research progress in helicopter rotor aeroacoustics noise is described, including new progress in the effects of atmosphere, ground and flight trajectory on the rotor aerodynamic noise, and the methods for calculating the acoustic scattering field of helicopter fuselage and maneuvering noise. The main work of the research on aerodynamic noise of the helicopter rotor is concluded and some prospects are also presented.

Key words: helicopter, rotor noise, blade vortex interaction noise, high speed impulsive noise, noise reduction technology, fuselage acoustic scattering field, maneuvering noise

中图分类号:

V211.52

徐国华, 史勇杰, 招启军, 王阳, 樊枫. 直升机旋翼气动噪声的研究新进展[J]. 航空学报, 2017, 38(7): 520991-520991.

XU Guohua, SHI Yongjie, ZHAO Qijun, WANG Yang, FAN Feng. New research progress in helicopter rotor aerodynamic noise[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(7): 520991-520991.

参考文献

[1] BRENTNER K S, FARASSAT F. Modeling aerodynamically generated sound of helicopter rotors[J]. Progress in Aerospace Sciences, 2003, 39(2-3): 83-120.
[2] JOHNSON W. Helicopter theory[M]. Princeton: Princeton University Press, 1980.
[3] GEORGE A R. Helicopter noise: State-of-the-art[J]. Journal of Aircraft, 1978, 15(11): 707-715.
[4] STERNFELD H. Advanced rotorcraft noise: AIAA-1980-0857[R]. Reston: AIAA, 1980.
[5] 吴希明. 我国直升机外部噪声控制技术发展思路研究[J]. 直升机技术, 2014(3): 1-6. WU X M. Research on the development path of the helicopter external noise control technology in China[J]. Helicopter Technique, 2014(3): 1-6 (in Chinese).
[6] BRENTNER K S, FARASSAT F. Helicopter noise prediction: The current status and future direction[J]. Journal of Sound and Vibration, 1994, 170(1): 79-96.
[7] BRENTNER K S. An efficient and robust method for predicting helicopter high-speed impulsive noise[J]. Journal of Sound and Vibration, 1997, 203(1): 87-100.
[8] ALLONGUE M, MARZE H J, POTDEVIN F. The quiet helicopter: From research to reality[C]//Proceedings of 55th Annual Forum of the American Helicopter Society, 1999.
[9] GUTIN L. On the sound of a rotating airscrew: NACA TM-1192[R]. Washington, D.C.: NASA, 1948.
[10] DEMING A F. Noise from propellers with symmetrical sections at zero blade angle, Ⅱ: NACA-TN-679[R]. Washington, D.C.: NACA, 1938.
[11] GARRICK I E, WATKINS C E. A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers: NACA-TR-1198[R]. Washington, D.C.: NACA, 1954.
[12] LOWSON M V. The sound field of singularities in motion[J]. Proceedings of the Royal Society of London, Series A, Mathematical and Physical Sciences, 1965, 286(1407): 559-572.
[13] WRIGHT S E. Sound radiation from a lifting rotor generated by asymmetric disc loading[J]. Journal of Sound and Vibration, 1969, 9(2): 223-240.
[14] LOWSON M V, OLLERHEAD J B. A theoretical study of helicopter rotor noise[J]. Journal of Sound and Vibration, 1969, 9(2):197-222.
[15] WILLIAMS J E F, HAWKINGS D L. Sound generation by turbulence and surfaces in arbitrary motion[J]. Philosophical Transactions for the Royal Society of London, Series A, Mathematical and Physical Sciences, 1969, 264(1151): 321-342.
[16] BRENTNER K S, FARASSAT F. An analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces[C]//Proceedings of 53rd Annual Forum of American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 1997.
[17] FARASSAT F. Theory of noise generation from moving bodies with an application to helicopter rotors: NASA-TR-R-451[R]. Washington, D.C.: NASA, 1975.
[18] FARASSAT F, BRENTNER K S. The uses and abuses of the acoustic analogy in helicopter rotor noise prediction[J]. Journal of American Helicopter Society, 1988, 33(1):29-36.
[19] FARASSAT F. Derivation of formulations 1 and 1A of Farassat: NASA/TM-2007-214853[R]. Washington, D.C.: NASA, 2007.
[20] BRENTNER K S. Prediction of helicopter rotor discrete frequency noise: A computer program incorporating realistic motions and advanced acoustic formulation: NASA-TM-87721[R]. Washington, D.C.: NASA, 1986.
[21] BRENTNER K S, BRES G A, PEREZ G, et al. Maneuvering rotorcraft noise prediction: A new code for a new problem[C]//Proceedings of AHS Aerodynamics, Acoustics, and Test Evaluation Technical Specialist Meeting. Alexandria, VA: American Helicopter Society International, Inc., 2002.
[22] FARASSAT F. Extension of Kirchhoff’s formula to radiation from moving surfaces[J]. Journal of Sound and Vibration, 1988, 123(3): 451-460.
[23] FRANCESCANTONIO P. A new boundary integral formulation for the prediction of sound radiation[J]. Journal of Sound and Vibration, 1997, 202(4): 491-509.
[24] 段广战, 陈平剑. 直升机旋翼厚度噪声研究[J]. 直升机技术, 2007(1): 6-10. DUAN G Z, CHEN P J. Research of helicopter rotor thickness noise[J]. Helicopter Technique, 2007(1): 6-10 (in Chinese).
[25] GOPALAN G, SCHMITZ F H. Understanding far field near-in-plane high speed harmonic helicopter rotor noise in hover: Governing parameters and design trends[C]//Proceedings of 64th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2008.
[26] 宋文萍, 韩忠华, 王立群, 等. 旋翼桨尖几何形状对旋翼气动噪声影响的定量计算分析[J]. 计算物理, 2001, 18(6): 569-572. SONG W P, HAN Z H, WANG L Q, et al. The effect of blade-tip shape on rotor aeroacoustic noise by Euler/Kirchhoff method[J]. Chinese Journal of Computational Physics, 2001, 18(6): 569-572 (in Chinese).
[27] 徐国华, 王适存. 具有后掠桨尖的旋翼气动特性计算方法[J]. 空气动力学学报, 1999, 17(3): 356-361. XU G H, WANG S C. An analytical method for predicting aerodynamic characteristics of the rotor with a swept tip[J]. Acta Aerodynamica Sinica, 1999, 17(3): 356-361 (in Chinese).
[28] SCHMITZ F H, GOPALAN G. High-speed impulsive helicopter noise reduction possibilities through on-blade acoustic control[C]//Proceedings of the International Forum on Rotorcraft Multidisciplinary Technology, 2007.
[29] SARGENT D C, SCHMITZ F H. Fundamental experimental studies supporting on blade tip air blowing control of in-plane rotor harmonic noise[C]//18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference). Reston: AIAA, 2012.
[30] KUEFMANN P, BARTELS R, KESSLER C, et al. On the design and development of a multiple-swashplate control system for the realization of individual blade control (IBC) for helicopters[C]//Proceedings of 67th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2011.
[31] SCHMITZS F H, BOXWELL D A, VERTICA W R, et al. Model-rotor high-speed impulsive noise: Full-scale comparisons and parametric variations[C]//Proceedings of 39th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 1983.
[32] 叶靓. 基于非结构网格的直升机旋翼流场及噪声研究[D]. 南京: 南京航空航天大学, 2009. YE L. Research on the flowfield and noise of helicopter rotors based on unstructured mesh[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2009 (in Chinese).
[33] 樊枫. 直升机非定常干扰流场与声场的计算方法研究与应用[D]. 南京: 南京航空航天大学, 2013. FAN F. Research and application of computational methods for unsteady flow field and sound field of helicopter[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2013 (in Chinese).
[34] 招启军, 徐国华. 基于Navier-Stokes方程/自由尾迹/全位势方程的旋翼流场模拟混合方法[J]. 空气动力学学报, 2006, 24(1): 15-21. ZHAO Q J, XU G H. A hybrid method based on Navier-Stokes/free wake/full-potential solver for rotor flow simulations[J]. Acta Aerodynamica Sinica, 2006, 24(1): 15-21 (in Chinese).
[35] 韩忠华, 宋文萍, 乔志德. 基于FW-H方程的旋翼气动声学计算研究[J]. 航空学报, 2003, 24(5): 400-404. HAN Z H, SONG W P, QIAO Z D. Aeroacoustic calculation for helicopter rotor in hover and in forward flight based on FW-H equation[J]. Acta Aeronautica et Astronautica Sinica, 2003, 24(5): 400-404 (in Chinese).
[36] 韩忠华, 宋文萍, 乔志德, 等. 应用于跨声速旋翼气动声学计算的两种时域方法的比较[J]. 航空学报, 2006, 27(5): 756-762. HAN Z H, SONG W P, QIAO Z D, et al. Comparison of time-domain prediction methods for transonic aeroacoustic noise generated by helicopter rotors[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(5): 756-762 (in Chinese).
[37] 解福田, 韩忠华, 宋文萍. 基于FW-Hpds方法的直升机旋翼气动噪声指向性分析[J]. 直升机技术, 2007(1): 11-15. XIE F T, HAN Z H, SONG W P. The analysis of the directivity of helicopter rotor noise based on a new acoustic method[J]. Helicopter Technique, 2007(1): 11-15 (in Chinese).
[38] WIDNALL S E. Helicopter noise due to blade-vortex interactions[J]. Journal of Acoustical Society of America, 1971, 50(1): 354-365.
[39] LEWY S, CAPLOT M. Review of some theoretical and experimental studies on helicopter rotor noise[J]. Vertica, 1984, 8(4): 309-321.
[40] 尹坚平, 胡章伟. 由计算的三元非定常压力数据来预估旋翼辐射的桨涡干扰噪声[J]. 航空学报, 1996, 17(6): 86-90. YIN J P, HU Z W. Prediction of rotor blade-vortex interaction noise using 3D unsteady surface pressure[J]. Acta Aeronautica et Astronautica Sinica, 1996, 17(6): 86-90 (in Chinese).
[41] 乔渭阳, 唐狄毅, 李文兰. 旋翼BVI噪声的理论模拟与分析[J]. 航空学报, 1994, 15(6): 725-730. QIAO W Y, TANG D Y, LI W L. Theoretical study on the blade-vortex interaction noise of helicopter rotor[J]. Acta Aeronautica et Astronautica Sinica, 1994, 15(6): 725-730 (in Chinese).
[42] MUNSKY B, GANDHI F. Analysis of helicopter blade-vortex interaction noise with flight path or attitude modification[J]. Journal of the American Helicopter Society, 2005, 50(2): 123-137.
[43] ALGERMISSEN G, WANGER S. Computation of helicopter BVI noise by coupling free-wake, Euler and Kirchhoff Method: AIAA-1998-2238[R]. Reston: AIAA, 1998.
[44] OH W S, JO K W, KWON O J. Two-dimensional BVI revisited using unstructured dynamic meshes[C]//Proceedings of 58th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2002.
[45] CARADONNA F X, STRAWN R C, BRIDGE J O. An experimental and computational study of rotor-vortex interactions[J]. Proceedings of the 14th European Rotorcraft Forum, 1988, 12(4): 315-327.
[46] MALOVRH B, GANDHI F, TAUSZIG L. Sensitivity of helicopter BVI induced noise and vibration to variations in individual interaction-parameter[C]//Proceedings of 57th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2001.
[47] SCHMITZ F H, BOXWELL D A, DAHAN C, et al. A note on the general scaling of helicopter blade-vortex interaction noise[C]//Proceedings of 38th Annual Forum and Technology Display of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 1982.
[48] SAKOSWKY P C, CHARLES B D. Noise measurement test results of AH-1G operational loads survey: 299-099-831[R]. Bell Helicopter Co., 1976.
[49] BOXWELL D A, SCHMITZ F H, SPLETTSTOESSER W R, et al. Helicopter model rotor-blade vortex interaction impulsive noise: Stability and parametric variations[J]. Journal of the American Helicopter Society, 1987, 32(1): 3-12.
[50] LOWSON M V. Focusing of helicopter BVI noise[J]. Journal of Sound and Vibration, 1996, 190(3): 477-494.
[51] RINGLER T D, GEORGE A R, STEELE J B. A study of blade-vortex interaction sound generation and directionality[C]//Proceedings of Technical Specialists’ Meeting on Rotorcraft Acoustics/Fluid Dynamics. Alexandria, VA: American Helicopter Society, International, Inc., 1991.
[52] WERNICKE R K, DREES J M. Second harmonic control[C]//Proceedings of the 19th Annual National Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 1963.
[53] WOOD E R, POWERS R W, CLINE J H, et al. On developing and flight testing a higher harmonic control system[J]. Journal of the American Helicopter Society, 1985, 30(1): 3-20.
[54] SPLETTSTOESSER W R, SCHULTZ K J, KUBE R, et al. A higher harmonic control test in the DNW to reduce impulsive BVI noise[J]. Journal of the American Helicopter Society, 1994, 39(4): 3-13.
[55] HAM N. A simple system for helicopter individual-blade-control and its application to gust alleviation[C]//Proceedings of the 6th European Rotorcraft Forum, 1980.
[56] HAM N, BEHAL B L, MCKILLIP R. Helicopter rotor lag damping augmentation through individual-blade-control[J]. Vertica, 1983, 7(4): 361-371.
[57] QUACKENBUSH T R. Testing of a stall flutter suppression system for helicopter rotors using individual-blade-control[J]. Journal of the American Helicopter Society, 1994, 29(3): 38-44.
[58] NORMAN T R, THEODORE C, SHINOD P, et al. Full-scale wind tunnel test of a UH-60 individual blade control System for performance improvement and vibration, loads and noise control[C]//Proceedings of the 65th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2009.
[59] RICHTER P, BLAAS A. Full scale wind tunnel investigation of an individual blade control (IBC) system for the BO 105 hingeless rotor[C]//Proceedings of the 19th European Rotorcraft Forum, 1980.
[60] JACKLIN S A, SWANSON S, BLAAS A, et al. Investigation of a helicopter individual blade control (IBC) system in two full-scale wind tunnel tests: NASA TP-2003-212276+7[R]. Washington, D.C.: NASA, 2003.
[61] TEVES D, KLOEPPEL V, RICHTER P. Development of active control technology in the rotating system, flight testing and theoretical investigations[C]//Proceedings of the 18th European Rotorcraft Forum, 1992.
[62] KESSLER C, FURST D, ARNOLD U. Open loop flight test results and closed loop status of the IBC-System on the CH-53G helicopter[C]//Proceedings of the 59th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2003.
[63] FURST D, KESSLER C. Closed loop IBC-System and flight test results on the CH-53G helicopter[C]//Proceedings of the 60th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2004.
[64] ROTH D. Advanced vibration reduction by IBC technology[C]//Proceedings of the 30th European Rotorcraft Forum, 2004.
[65] STRAUB F K, ANAND V R, BIRCHETTE T S, et al. Wind tunnel tests of the SMART active flap rotor[C]//Proceedings of the 65th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2009.
[66] BROOKS T F, BURLEY C L. Rotor broadband noise prediction with comparison to model data: AIAA-2001-2210[R]. Reston: AIAA, 2001.
[67] BROOKS T F, BURLEY C L. Blade wake interaction noise for a model main rotor[C]//Proceedings of the 53rd Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 1997.
[68] AMIET R K. Acoustic radiation from an airfoil in a turbulent stream[J]. Journal of Sound and Vibration, 1975, 41(4): 407-420.
[69] BURLEY C L, BROOKS T F, CHARLES B D, et al. Tiltrotor aeroacoustic code (TRAC) prediction assessment and initial comparisons with tram test data[C]//Proceedings of the 25th European Rotorcraft Forum, 1999.
[70] BURLEY C L, BROOKS T F, MARCOLINI M M, et al. Tiltrotor aeroacoustic code (TRAC) predictions and comparisons with measurements[J]. Journal of the American Helicopter Society, 2000, 45(2):80-89.
[71] CASPAR J, FARASSAT F. A new time domain formulation for broadband noise predictions[J]. International Journal of Aeroacoustics, 2002, 1(3): 207-240.
[72] DELANY M E, BAZLEY E N. A note on the effect of ground absorption in the measurement of aircraft noise[J]. Journal of Sound and Vibration, 1971, 16(3): 315-322.
[73] WEIR D S, JUMPER S J, et al. Aircraft noise prediction program theoretical manual: rotorcraft system noise prediction system, Part 4: NASA-TM-83199[R]. Washington, D.C.: NASA, 1995.
[74] ZORUMSKI W E. Aircraft noise prediction program theoretical manual, Part 1: NASA-TM-83199[R]. Washington, D.C.: NASA, 1982.
[75] EVANS L B, BASS H E, SUTHERLAND L C. Atmospheric absorption of sound: Theoretical predictions[J]. Journal of the Acoustic Society of America, 1972, 51(5B): 1565-1575.
[76] 王阳. 直升机旋翼气动噪声的计算及降噪方法研究[D].南京: 南京航空航天大学, 2010. WANG Y. Research on calculation and debasement method of rotor aerodynamic noise for helicopters[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010 (in Chinese).
[77] ATTENBOROUGH K. Acoustical impedance models for outdoor ground surfaces[J]. Journal of Sound and Vibration, 1985, 99(4): 521-544.
[78] GOPALAN G, XUE M, ATKINS E M, et al. Longitudinal-plane simultaneous non-interfering approach trajectory design for noise minimization[C]//Proceedings of the 59th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2003.
[79] HAWLES D R. Flight operations to minimize noise[C]//Proceedings of the 26th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 1970.
[80] EDWARDS B D. XV-15 tiltrotor aircraft noise characteristics[C]//Proceedings of the 46th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc.,1990.
[81] HINDSON W S, CHEN R T N. Operational tests for noise abatement approaches for rotorcraft using differential GPS for guidance[J]. Journal of the American Helicopter Society, 1998, 43(4): 352-359.
[82] CONNER D A, MARCOLINI M A, DECKER W A, et al. XV-15 tiltrotor low noise approach operations[C]//Proceedings of the 55th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc.,1999.
[83] LAPPOS N, ARNOLD J, ERWAY P, et al. The development of a decelerating helicopter instrument landing system using differential GPS[C]//Proceedings of the 56th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2000.
[84] CONNER D A, EDWARDS B D, DECKER W A, et al. NASA/Army/Bell XV-15 tiltrotor low noise terminal area operations flight research program[C]//Proceedings of 53rd Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 1997.
[85] SCHMITZ F H. Reduction of blade-vortex interaction (BVI) noise through X-Force control[J]. Journal of the American Helicopter Society, 1998, 43(1): 14-24.
[86] GOPALAN G, SCHMITZ F H, FREDRIC H, et al. Flight path management and control methodology to reduce helicopter blade-vortex interaction (BVI) noise[C]//Proceedings of 56th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2000.
[87] GOPALAN G, FREDRIC H, SCHMITZ F H. Flight path control of helicopter blade-vortex interaction noise in the presence of wind[D]. Maryland: University of Maryland, 2001.
[88] YU Y H. Rotor blade-vortex interaction noise[J]. Progress in Aerospace Sciences, 2000, 36(2): 97-115.
[89] CHEHAB M, WÖLK J. A wind tunnel study of X-Force generators to reduce helicopter blade-vortex interaction (BVI) noise[C]//Proceedings of the AIAA Student Design Conference, 2000.
[90] EDWARDS B, COX C. Revolutionary concepts for helicopter noise reduction: SILENT program: NASA/CR-2002-211650[R]. Washington, D.C.: NASA, 2002.
[91] BRIAN M, FARHAN G, LIONEL T. An analysis of helicopter blade-vortex interaction noise with flight path or attitude modification[R]. Pennsylvania: The Pennsylvania State University, 2002.
[92] LEE S K, BRENTNER K S, MORRIS P J. Prediction of acoustic scattering in the time domain using a moving equivalent source method: AIAA-2009-3177[R]. Reston: AIAA, 2009.
[93] FARASSAT F. Open rotor noise prediction at NASA Langley-capabilities, research and development: NASA TM-2010-216178[R]. Washington, D.C.: NASA, 2010.
[94] LEE S K. Prediction of acoustic scattering in the time domain and its applications to rotorcraft noise[D]. State College, PA: The Pennsylvania State University, 2009.
[95] HARDIN J, HUSSAINI M Y. Computational aeroacoustics[M]. New York: Springer, 1993.
[96] TAM C K W. Computational aeroacoustics: Issues and methods[J]. AIAA Journal, 1995, 33(10): 1788-1796.
[97] LONG L N, MORRIS P J, AHUJA V, et al. Several aerospace applications of computational aeroacoustics[C]//Proceedings of the ASME Noise Control and Acoustics Division, 1998, 25: 13-20.
[98] CHEN L H, SCHWEIKERT D G. Sound radiation from an arbitrary body[J]. Journal of the Acoustical Society of America, 1963, 35(1): 1626-1632.
[99] BURTON A J, MILLER G F. The application of integral equation methods to the numerical solution of some exterior boundary-value problems[J]. Proceedings of the Royal Society, Series A, Mathematical and Physical Sciences, 1971, 323(1553): 201-210.
[100] SEYBERT A F, SOENARKO B, RIZZO F J. An advanced computational method for radiation and scattering of acoustic waves in three dimensions[J]. Journal of the Acoustical Society of America, 1985, 77(2): 362-368.
[101] MYERS M K, HAUSMANN J S. Computational of acoustic scattering from a moving rigid surface[J]. Journal of the Acoustical Society of America, 1992, 91(5): 2594-2605.
[102] GENNARETTI M, IEMMA U, TESTA C. Prediction of sound scattered by moving bodies with applications to propeller-driven airplanes: AIAA-2006-2475[R]. Reston: AIAA, 2006.
[103] TESTA C, IANNIELLO S, BERNARDINI G, et al. Sound scattered by a helicopter fuselage in descent flight condition: AIAA-2007-3497[R]. Reston: AIAA, 2007.
[104] ATALLA N, GLEGG S A L. A ray-acoustics approach to fuselage scattering of rotor noise: AIAA-1990-4013-CP[R]. Reston: AIAA, 1990.
[105] TINETTI A F, DUNN M H. Aeroacoustics noise prediction using the fast scattering code: AIAA-2005-3061[R]. Reston: AIAA, 2005.
[106] DUNN M H, TINETTI A F. Application of fast multipole methods to the NASA fast scattering code: AIAA-2008-2875[R]. Reston: AIAA, 2008.
[107] TINETTI A F, DUNN M H. Fast scattering code (FSC) user’s manual: Version 2.0: NASA/CR-2006-214510[R]. Washington, D.C.: NASA, 2006.
[108] DUNN M H, TINETTI A F. Aeroacoustic scattering via the equivalent source method: AIAA-2004-2937[J]. Reston: AIAA, 2004.
[109] LEE S, BRENTNER K S, MORRIS P J. Time-domain approach for acoustic scattering of rotorcraft noise[C]//Proceedings of 65th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2009.
[110] BRENTNER K S, JONES H E. Noise prediction for maneuvering rotorcraft: AIAA-2000-2031[R]. Reston: AIAA, 2000.
[111] CHEN H N, BRENTNER K S, LOPES L V, et al. A study of rotorcraft noise prediction in maneuvering flight: AIAA 2004-850[R]. Reston: AIAA, 2004.
[112] BRENTNER K S, PEREZ G, BRES G A, et al. Toward a better understanding of maneuvering rotorcraft noise[C]//Proceedings of 58th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2002.
[113] SITARAMAN J, ROGET B. Prediction of helicopter maneuver loads using a fluid-structure analysis[J]. Journal of Aircraft, 2009, 46(5): 1770-1784.
[114] JANAKIRAM R D, KHAN H. Prediction and validation of helicopter descent flyover noise[C]//Proceedings of 56th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2000.
[115] HENNES C C, CHEN H N, BRENTNER K S, et al. Influence of transient flight maneuvers on rotor wake dynamics and noise radiation[C]//Proceedings of 60th Annual Forum of the American Helicopter Society. Alexandria, VA: American Helicopter Society International, Inc., 2004.
[116] CHEN H N, BRENTNER K S, ANANTHAN S, et al. A computational study of helicopter rotor wakes and noise generated during transient maneuvers[J]. Journal of the American Helicopter Society, 2008, 53(1):37-55.the AIAA Student Design Conference, 2000.
[44] Schmitz F H, Gopalan G, Sim B-C, Flight Trajectory Management to Reduce Helicopter Blade-Vortex Interac-tion(BVI) Noise with Head/Tailwind Effects, Proceedings of the 26th European Rotorcraft Forum, 2000.
[45] Kuo B C, Sim B W-C, Schmitz F H, Blade-Vortex In-teraction Wave Radiation Patterns of Helicopter Blades With Different Leading-Edge Geometry, Proceedings of the American Helicopter Society 58th Annual Forum, 2002.
[46] Schmitz F. H., Boxwell D. A., Splettstoesser W. R., et al., Model-rotor high-speed impulsive noise: full-scale comparisons and parametric variations. Vertica, 1984, 8(4): 395-422.
[47] Lele S. G., Computational aeroacoustics: A review. AIAA 97-0018, 1997.
[48] 韩忠华, 宋文萍, 乔志德, Kirchhoff 方法在旋翼前飞噪声预测中的应用研究. 空气动力学学报, 2004, 22(2): 47-51.
[49] 宋文萍, 韩忠华, 王立群等, 旋翼桨尖几何形状对旋翼气动噪声影响的定量计算分析, 计算物理,2001, 18(6):569~572.
[50] 叶靓，基于非结构网格的直升机旋翼流场及噪声研究. 博士学位论文, 南京航空航天大学, 2009.
[51] 樊枫，直升机非定常干扰流场与声场的计算方法研究与应用.博士学位论文，南京航空航天大学，2013.
[52] 招启军, 徐国华, 基于Navier-Stokes方程/自由尾迹/全位势方程的旋翼流场模拟混合方法, 空气动力学学报, 2006, 24(1):15-21.
[53] Hau-Tak Rudy Chou, A Study of Rotor Broadband Noise Mechanisms and Helicopter Tail Rotor Noise, Cornell University, Ithaca, New York. NAG2-379,August 1990.
[54] George.R.,Shau-Tak Chou, Broadband Rotor Noise Analyses, Scientific and Technical Information Of-fice,1984.
[55] S. Léwy., Computation of broadband noise radiated by a ducted fan, 8th International Congress on Sound and Vibration Hong Kong (Chine), July 02-06, 2001.
[56] Ulrich W. Ganz, Paul D. Joppa, Timothy J. Patten, and Daniel F. Scharpf., Boeing 18-Inch Fan Rig Broad-band Noise Test, Boeing Commercial Airplane Group, Seattle, Washington, September 1998.
[57] 方丹群，“空气动力性噪声与消声器”，科学出版社，1978.
[58] Prichard D S, Boyd D D, Burley C L, NASA/Langley's CFD-Based BVI Rotor Noise Prediction Systems: (ROTORNET/FPRBVI) An Introduction and User's Guide, NASA TM-109147, 1994.
[59] Farassat F, Succi G P, The Prediction of Helicopter Rotor Discrete Frequency Noise, Vertica, 1983, 7(4):309~320.
[60] Brentner K S, Prediction of Helicopter Rotor Discrete Frequency Noise—A Computer Program Incorporating Realistic Motions and Advanced Acoustic Formulation, NASA TM-87721, 1986.
[61] Brentner K S, Brès G A, Perez G. et al., Maneuvering Rotorcraft Noise Prediction: A New Code for a New Problem, Proceedings of the AHS Aerodynamics, Acous-tics, and Test Evaluation Specialist Meeting, 2002.
[62] 王阳，直升机旋翼气动噪声的计算及降噪方法研究.博士学位论文,南京航空航天大学,2010.
[63] Delany M E, Bazley E N, A Note on the Effect of Ground Absorption in The Measurement of Aircraft Noise, Journal of Sound and Vibration, 1971, 16(3):315~322.
[64] Weir D, Jumper S, et al, Aircraft Noise Prediction Pro-gram Theoretical Manual: Rotorcraft System Noise Pre-diction System , NASA-TM-83199, 1995.
[65] William E Z, Aircraft Noise Prediction Program Theo-retical Manual, NASA-TM-83199, 1982.
[66] Evans L B, Bass H E, Sutherland L C, Atmospheric Absorption of Sound: Theoretical Predictions, Journal of Acoustic Society of America, 1972, 51(5B): 1565~1575.
[67] Attenborough K, Acoustical Impedance Models for Out Door Ground Surfaces, Journal of Sound and Vibra-tion, 1985, 99(4), 521~544.
[68] Bryan Edwards, Charles Cox, Revolutionary Concepts for Helicopter Noise Reduction-SILENT Program, NASA-CR-2002-211650, 2002.
[69] Shahady P A, e al, The Effects of Modulated Blade Spacing on Static Rotor Acoustics and Performance, AIAA-1973-1020, 1973.
[70] Schmitz F H, Gopalan G, Sim B W, Flight Path Man-agement and Control Methodology to Reduce Helicopter Blade-Vortex Interaction (BVI) Noise, Journal of Aircraft, 2002, 39(2):193~204.
[71] Gopalan G and Schmitz F H , Understanding Far Field Near-in-plane High Speed Harmonic Helicopter Rotor Noise in Hover: Governing Parameters and Design Trends, Proceeding of the AHS Technical Specialists Conference,2008.
[72] Schmitz F H and Gopalan G, High-speed Impulsive Helicopter Noise Reduction Possibilities Through On-Blade Acoustic Control, Proceeding of the International Forum on Rotorcraft Multidisciplinary Technology, 2007.
[73] Lee S., Brentner K. S., Morris P. J., Prediction of Acoustic Scattering in the Time Domain Using a Moving Equivalent Source Method. AIAA 2009-3177, 2009.
[74] Farassat F., Open Rotor Noise Prediction at NASA Langley-Capabilities, Research and Development. NASA TM-2010-216178, 2010.
[75] Lee S., Prediction of acoustic scattering in the time domain and its applications to rotorcraft noise. Doctor-al Dissertation, The Pennsylvania State University, 2009.
[76] Atalla N., Glegg S., A Ray-Acoustics Approach to Fu-selage Scattering of Rotor Noise. AIAA 90-4013, 1990.
[77] Atalla N., Glegg S., Ray-Acoustics Approach to Fuse-lage Scattering of Rotor Noise.Journal of the American Helicopter Society,1993,38(3):56-63.
[78] Tinetti A. F., Dunn M. H., Aeroacoustics noise prediction using the fast scattering code. AIAA 2005-3061, 2005.
[79] Dunn M. H., Tinetti A. F., Application of Fast Multipole Methods to the NASA Fast Scattering Code. AIAA 2008-2875, 2008.
[80] Tinetti A. F., Dunn M. H., Fast Scattering Code(FSC) User’s Manual(Version 2.0). NASA CR-2006-214510, 2006.
[81] Dunn M. H., Tinetti A. F., Aeroacoustic Scattering Via the Equivalent Source Method. AIAA 2004-2937, 2004.
[82] Lee S., Erwin J. P., Brentner K. S., A Method to Predict Acoustic Scattering of Rotorcraft Noise. Journal of the American Helicopter Society, 2009, 54(4):1-15.
[83] Lee S., Brentner K. S., Morris P. J., Time-Domain Ap-proach for Acoustic Scattering of Rotorcraft Noise. American Helicopter Society 64th Annual Forum Pro-ceedings, Texas, 2009.
[84] 陈平剑，仲唯贵，段广战，直升机气动噪声研究进展，实验流体力学，2015, 29(3): 18~24.
[85] 吴希明，我国直升机外部噪声控制技术发展思路研究，直升机技术，2014， No.3: 1~6.
[86] 李琪娜，直升机主旋翼的气动和噪声计算.硕士学位论文，北京航空航天大学，2002.

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直升机旋翼气动噪声的研究新进展

New research progress in helicopter rotor aerodynamic noise

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