| [1] Green J E. Air travel-greener by design mitigating the environmental impact of aviation: opportunities and priorities[J]. The Aeronautical Journal, 2005, 109(1099): 495-510.[2] Green J E. Civil aviation and the environment—the next frontier for the aerodynamicist[J]. The Aeronautical Journal, 2006, 110(1110): 469-486.[3] Epstein A H. Aeropropulsion for commercial aviation in the 21st century and research directions needed, AIAA-2013-0001[R]. Reston: AIAA, 2013.[4] Qiao W Y. Aeroacoustics of aeroengine[M]. Beijing: Beihang University Press, 2010 (in Chinese). 乔渭阳. 航空发动机气动声学[M]. 北京: 北京航空航天大学出版社, 2010.[5] Josling R D, Thomas R H, Choudhari M M. Synergism of flow and noise control technologies[J]. Progress in Aerospace Sciences, 2005, 41(5): 363-417.[6] Dowling A, Greiter E D. The silent aircraft initiative—overview, AIAA-2007-0452[R]. Reston: AIAA, 2007.[7] Zhu Z Q, Wang X L, Wu Z C, et al. Discussion of design methods for silent and fuel efficient medium range civil transport[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(3): 562-572 (in Chinese). 朱自强, 王晓璐, 吴宗成, 等. 高经济性静音中航程民用机设计方法讨论[J]. 航空学报, 2008, 29(3): 562-572.[8] Dobrzynski W. Almost 40 years of airframe noise research: what did we achieve?[J]. Journal of Aircraft, 2010, 47(2): 353-367.[9] Dobrzynski W, Buchholz H. Full-scale noise testing on airbus landing gears in the German-Dutch wind tunnel, AIAA-1997-1597[R]. Reston: AIAA, 1997.[10] Stoker R W, Guo Y, Streett C, et al. Airframe noise source locations of a 777 aircraft in flight and comparisons with past model scale tests, AIAA-2003-3232[R]. Reston: AIAA, 2003.[11] Long S L, Nie H, Xue C J, et al. Simulation and experiment on aeroacoustic noise characteristics of aircraft landing gear[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(6): 1002-1013 (in Chinese). 龙双丽, 聂宏, 薛彩军, 等.飞机起落架气动噪声特性仿真与试验[J]. 航空学报, 2012, 33(6): 1002-1013.[12] Ravetta P A, Burdisso R A, Ng W F. Wind tunnel aeroacoustic measurements of a 26% scale 777 main landing gear model, AIAA-2004-2885[R]. Reston: AIAA, 2004.[13] Jaeger S M, Burnside N J, Soderman P T, et al. Microphone array assessment of an isolated 26%-scale, high-fidelity landing gear, AIAA-2002-2410[R]. Reston: AIAA, 2002.[14] Horne W C, James K D, Arledge T K, et al. Measurements of 26% scale 777 airframe noise in the NASA Ames 40 by 80 Foot Wind tunnel, AIAA-2005-2810[R]. Reston: AIAA, 2005.[15] Smith M G, Fenech B, Chow L C, et al. Control of noise sources on aircraft landing gear bogies, AIAA-2006-2626[R]. Reston: AIAA, 2006.[16] Hayes J A, Horne W C, Soderman P T, et al. Airframe noise characteristics of a 4.7% scale DC-10 model, AIAA-1997-1594[R]. Reston: AIAA, 1997.[17] Dobrzynski W, Nagakura K, Gehlhar B, et al. Airframe noise studies on wings with deployed high-lift devices, AIAA-1998-2337[R]. Reston: AIAA, 1998.[18] Herkes W H, Stoker R W. Wind tunnel measurements of the airframe noise of a high-speed civil transport, AIAA-1998-0472[R]. Reston: AIAA, 1998.[19] Davy R, Remy H. Airframe noise characteristics of a 1/11 scale airbus model,AIAA-1998-2335[R]. Reston: AIAA, 1998.[20] Dobrzynski W, Gehlhar B, Buchholz H. Model- and full scale high-lift wing wind tunnel experiments dedicated to airframe noise reduction[J]. Aerospace Science Technology, 2001, 5(1): 27-33.[21] Choudhari M M, Khorrami M. Slat cove unsteadiness: effect of 3D flow structures, AIAA-2006-0211[R]. Reston: AIAA, 2006.[22] Dobrzynski W, Pott-Pollenske M. Slat noise source studies for farfield noise prediction, AIAA-2001-2158[R]. Reston: AIAA, 2001.[23] Streett C L. Numerical simulation of fluctuations leading to noise in a flap-edge flowfield, AIAA-1998-0628[R]. Reston: AIAA, 1998.[24] Radezrsky R H, Singer B A, Khorrami M R. Detailed measurements of a flap side-edge flow field, AIAA-1998-0700 [R]. Reston: AIAA, 1998.[25] Brooks T F, Humphreys W M, Jr. Flap edge aeroacoustic measurements and predictions, AIAA-2000-1975[R]. Reston: AIAA, 2000.[26] Li Y, Wang X N, Zhang D J. Control strategies for aircraft airframe nose reduction[J]. Chinese Journal of Aeronautics, 2013, 26(2): 249-260.[27] Zhu Z Q, Wu Z C, Chen Y C, et al. Advanced technology in aerodynamic design of commercial aircraft[M]. Shanghai: Shanghai Jiao Tong University Press, 2013 (in Chinese). 朱自强, 吴宗成, 陈迎春, 等. 民机空气动力设计先进技术[M]. 上海: 上海交通大学出版社, 2013.[28] Ravetta P, Burdisso R, Ng W, et al. Screening of potential noise control devices at virginia tech for QTD II flight test, AIAA-2007-3455[R]. Reston: AIAA, 2007.[29] Ravetta P, Burdisso R, Ng W. Noise control of landing gears using elastic membrane-based fairings, AIAA-2007-3466[R]. Reston: AIAA, 2007.[30] Abeysinghe A, Whitmire J, Nesthus D. QTD II main landing gear noise reduction fairing design and analysis, AIAA-2007-3456[R]. Reston: AIAA, 2007.[31] Elkoby R, Brusniak L, Stoker R, et al. Airframe noise test results from the QTD II flight test program, AIAA-2007-3457[R]. Reston: AIAA, 2007.[32] Dobrzynski W, Chow L C, Guion P, et al. European study on landing gear airframe noise sources, AIAA-2000-1971[R]. Reston: AIAA, 2000.[33] Chow L C, Mau K, Remy H. Landing gear and high lift devices airframe noise research, AIAA-2002-2408[R]. Reston: AIAA, 2002.[34] Piet J F, Davy R, Elias G, et al. Flight test investigation of add-on treatments to reduce aircraft airframe noise, AIAA-2005-3007[R]. Reston: AIAA, 2005.[35] Davy R, Moens P, Remy H. Aeroacoustic behaviour of a 1∶11 scale airbus model in the open anechoic wind tunnel CEPRA 19, AIAA-2002-2412[R]. Reston: AIAA, 2002.[36] Piet J F, Michel U, Bohning P. Localization of the acoustic sources of the A340 with a large phased microphone array during flight tests, AIAA-2002-2506[R]. Reston: AIAA, 2002.[37] Piet J F, Chow L C, Laporte F, et al. Flight test investigation of high-lift devices and landing gear modifications to achieve airframe noise reduction[C]//Proceedings of European Congress on Computational Methods in Applied Sciences and Engineering, 2004.[38] Dobrzynski W, Chow L C, Smith M, et al. Experimental assessment of low noise landing gear component design, AIAA-2009-3276[R]. Reston: AIAA, 2009.[39] Oerlemans S, Sandu C, Malin N, et al. Reduction of landing gear noise using meshes, AIAA-2010-3972[R]. Reston: AIAA, 2010.[40] Khorrami M R, Lockard D P. Effects of geometrical details on slat noise generation and propagation, AIAA-2006-2664[R]. Reston: AIAA, 2006.[41] Kolb A, Faulhaber R, Drobietz R,et al. Aeroacoustic wind tunnel study on a two dimensional high lift configuration, AIAA-2007-3447[R]. Reston: AIAA, 2007.[42] Imamura T, Ura H, Yokokawa Y, et al. Designing of slat cove filler as a noise reduction device for leading-edge slat, AIAA-2007-3473[R]. Reston: AIAA, 2007.[43] Pott-Pollenske M, Wild J, Nagel B, et al. Multidisciplinary design approach toward low noise high-lift devices [C]//Conference Proceedings of the 8th ONERA-DLR Aerospace Symposium (ODAS), 2007.[44] Shmilovich A, Yadlin Y, Pitera D M. Wing leading edge concepts for noise reduction[C]//27th International Congress of the Aeronautical Sciences, 2010.[45] Crighton D G. Airframe noise in aeroacoustics of flight vehicles[M]. Washington, D.C.: Acoustical Society of America, 1995.[46] Lockard D P, Lilley G M. The airframe noise reduction challenge, NASA-TM-2004-21303[R]. Washington, D.C.: NASA, 2004.[47] Singer B A, Guo Y. Development of computational aeroacoustics tools for airframe noise calculations[J]. International Journal of Computational Fluid Dynamic, 2004, 18(6): 455-469.[48] Wang M, Freund J B, Lele S K. Computational prediction of flow generated sound[J]. Annual Review of Fluid Mechanics, 2003, 38: 483-512.[49] Tam C K W. Computational aeroacoustics: an overview RTOAVT symposium on ageing mechanisms and control, part A, developments in computational aero- and hydro-acoustics[R]. 2001.[50] Farassat F, Casper J H. Towards an airframe noise prediction methodology, survey of current approaches, AIAA-2006-0210[R]. Reston: AIAA, 2006.[51] Dahl M. A process for assessing NASA's capability in aircraft noise prediction technology, AIAA-2008-2813[R]. Reston: AIAA, 2008.[52] Zorumski W E. Aircraft noise prediction program theoretical manual, Part I and II, NASA TM-83199[R]. Washington, D.C.: NASA, 1982.[53] Smith M G, Chow L C. Prediction method for aerodynamic noise from aircraft landing gear, AIAA-1998-2228[R]. Reston: AIAA, 1998.[54] Guo Y P. A semi-empirical model for aircraft landing gear noise prediction, AIAA-2006-2627[R]. Reston: AIAA, 2006.[55] Guo Y P, Yamamoto K J, Stoker R W. Component-based empirical model for high-lift system noise prediction[J]. Journal of Aircraft, 2003, 40(5): 914-922.[56] Lighthill M J. On sound generated aerodynamically. I. general theory[J]. Proceedings of the Royal Society of London, Series A: Mathematical and Physical Sciences, 1952, 211(1107): 564-587.[57] Ffowcs Williams J E, Hawkings D L. Sound generation by turbulence and surfaces in arbitrary motion[J]. Philosophical Transactions of the Royal Society of London, Series A: Mathematical and Physical Sciences, 1969, 264(1151): 321-342.[58] Yu L, Song W P, Han Z H, et al. Aeroacoustic noise prediction using hybrid RANS/LES method and FW-H equation[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(8): 1795-1805 (in Chinese). 余雷, 宋文萍, 韩忠华, 等. 基于混合RANS/LES方法与FW-H方程的气动声学计算研究[J]. 航空学报, 2013, 34(8): 1795-1805.[59] Wang F, Liu Q H, Cai J S. An unified computational aeroacoustic integral method of noise radiation and scattering with noncompact bodies[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(11): 2482-2491 (in Chinese). 王芳, 刘秋洪, 蔡晋生. 非紧致结构气动噪声辐射散射统一积分计算方法[J]. 航空学报, 2013, 34(11): 2482-2491.[60] Jefferies R. CLEEN program technologies developments[C]//NASA ERA N+2 Advanced Vehicle Concepts of Quck-starts NRA Pre-proposal Meeting, 2010.[61] Wisley C, Stoker R. Continuous lower energy, emissions and noise(CLEEN) technologies development[R]. 2010.[62] Collier F, Thomas R, Burley C, et al. Enviromentally responsible aviation-real solutions for environmental challenge facing aviation[C]//27th Congress of the International Council of the Aeronautical Sciences, 2010.[63] Reiman C A, Tinetti A F, Dunn M H. Noise scattering by the blended wing body airplane: measurements and prediction, AIAA-2006-3144[R]. Reston: AIAA, 2006.[64] Czech M J, Thomas R H, Elkoby R. Propulsion airframe aero-acoustic integration effects for a hybrid wing body aircraft configuration, AIAA-2010-3912[R]. Reston: AIAA, 2010.[65] Thomas R H, Burley C L, Olson E D. Hybrid wing body aircraft system noise assessment with propulsion airframe aero-acoustic experiments, AIAA-2010-3913[R]. Reston: AIAA, 2010.[66] Bradley M K, Droney C K. Subsonic ultra green aircraft research: Phase I: final peport, NASA/CR-2011-216847[R]. Washington, D.C.: NASA, 2011.[67] Bradley M K, Droney C K. Subsonic ultra green aircraft research, Phase II: N+4 advanced concept development, NASA/CR-2012-217556[R]. Washington, D.C.: NASA, 2012.[68] Li G Y, Zhang J P. Dual expectations on fight[J]. International Aviation, 2011(2): 47-50 (in Chinese). 李广义, 张晋平. 人类对飞行的双重追求[J]. 国际航空, 2011(2): 47-50.[69] Xu D K. "Clean Sky II" project in Europe aviation industry[J]. International Aviation, 2013(1): 60-62 (in Chinese). 徐德康. 欧洲航空工业制定"清洁天空II"计划[J]. 国际航空, 2013(1): 60-62.[70] Chen D B, Zhou J J, Hao X, et al. Review of aeroacoustic measurement techniques in wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(1): 106-112 (in Chinese). 陈大斌, 周家检, 郝璇, 等. 气动噪声风洞试验技术发展概述[J]. 实验流体力学, 2013, 27(1): 106-112. |
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