| Citation: | Experiment on active control of low frequency in-plane harmonic noise for electrically controlled rotor[J]. Journal of Aerospace Power, 2018, 33(12). doi: 10.13224/j.cnki.jasp.2018.12.015
|
| [1] |
SCHMITZ F H.The challenges and possibilities of a truly quiet helicopter［J］.Journal of the American Helicopter Society,2016,61(4):041001.1-041001.33
|
| [2] |
SCHMITZ F H,AGGARWAL H R,BOXWELL D A.Prediction measurement of a low-frequency harmonic noise of hovering model helicopter rotor［J］.Journal of Aircraft,2000,37(5):786-795.
|
| [3] |
SIM B W,JANAKIRAM R D,LAU B H.Reduced in-plane,low frequency noise of an active flap rotor［R］.Grapevine,Texas:American Helicopter Society 65th Annual Forum,2009.
|
| [4] |
冯剑波,陆洋,徐锦法,等.旋翼桨涡干扰噪声开环桨距主动控制研究［J］.航空学报,2014,35(11):2901-2909.FENG Jianbo,LU Yang,XU Jinfa,et al.Research on the effect of open loop active blade pitch control on rotor BVI noise alleviation［J］.Acta Aeronautica et Astronautica Sinica,2014,35(11):2901-2909.(in Chinese)
|
| [5] |
朱正,招启军.低HSI噪声旋翼桨叶外形优化设计方法［J］.航空学报,2015,36(5):1442-1452ZHU Zheng,ZHAO Qijun.Optimization design method for rotor blade-tip shape with low HSI noise characteristics［J］.Acta Aeronautics et Astronautica Sinica,2015,36(5):1442-1452.(in Chinese)
|
| [6] |
SARGENT D C,SCHMITZ F H.Fundamental experimental studies supporting on-blade tip air blowing control of in-plane rotor harmonic noise［R］.Colorado Springs:the 18th AIAA/CEAS Aeroacoustics Conference,2012.
|
| [7] |
SARGENT D C.Active jet acoustic control of low frequency,in plane helicopter harmonic noise［D］.College Park,MD:University of Maryland,2012.
|
| [8] |
BROOKS T F,BOOTH E R,JOLLY J R,et al.Reduction of blade-vortex interaction noise through higher harmonic pitch control［J］.Journal of the American Helicopter Society,1990,35(1):86-91.
|
| [9] |
KESSLER C,FUERST D,ARNOLD U T P.Open loop flight test results and closed loop status of the IBC system on the CH-53G helicopter［R］.Phoenix,AZ:American Helicopter Society 59th Annual Forum,2003.
|
| [10] |
PATT D,LIU L,FRIEDMANN P P.Helicopter noise reduction by actively controlled flaps［R］.Monterey,California:the 26th AIAA Aero Acoustics Conference,2005.
|
| [11] |
SIM B W.Suppressing in-plane,low frequency helicopter harmonic noise with active controls［R］.Fishermans Wharf,CA:American Helicopter Society San Francisco Bay Area Chapters Aeromechanics Specialists Meeting,2008.
|
| [12] |
SARGENT D C,GOPALAN G,SCHMITZ F H.Acoustic design and parametric variations,active acoustic control,and performance study of in-plane far-field helicopter rotor noise in forward flight［R］.Phoenix,AZ:American Helicopter Society 66th Annual Forum Proceedings,2010.
|
| [13] |
SARGENT D C,GOPALAN G,SCHMITZ F H.In-plane thickness and loading noise of helicopters in forward flight prediction and on-blade control through ideal in-plane force control［R］.Phoenix,AZ:American Helicopter Society 66th Annual Forum and Technology Display,2010.
|
| [14] |
陆洋,董维生,洪亮,等.基于自适应滤波的电控旋翼桨距控制试验［J］.航空动力学报,2012,27(12)：2706-2713.LU Yang,DONG Weisheng,HONG Liang,et al.Experiment on blade pitch control of electrically controlled rotor based on adaptive filter control algorithm［J］.Journal of Aerospace Power,2012,27(12)：2706-2713.(in Chinese)
|
| [15] |
陆洋,王超.电控旋翼气动特性建模与风洞试验验证［J］.航空动力学报,2013,28(1):60-66.LU Yang,WANG Chao.Aerodynamic characteristic modeling of electrically controlled rotor and wind tunnel test verification［J］.Journal of Aerospace Power,2013,28(1):60-66.(in Chinese)
|
| [16] |
董祥见.电控旋翼噪声主动控制试验研究［D］.南京:南京航空航天大学,2017.DONG Xiangjian.Experimental study on the active noise control of electronically controlled rotor［D］.Nanjing:Nanjing University of Aeronautics and Astronautics,2017.(in Chinese)
|
| [17] |
SHAW J,ALBION N,HANKER E J,et al.Higher harmonic control:wind tunnel demonstration of fully effective vibratory hub force suppression［J］.Journal of the American Helicopter Society,1989,34(1):14-25.
|
| [18] |
JACKLIN S A.Comparison of five system identification algorithms for rotorcraft higher harmonic control［R］.NASA TP-1998-207687,1998.
|
| [19] |
PATT D,LIU L,CHANDRASEKAR J,et al.High harmonic control algorithm for helicopter vibration reduction revisited［J］.Journal of Guidance,Control,and Dynamics,2005,28(5):918-930.
|
DownLoad: