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NTIS 바로가기Applied acoustics, v.188, 2022년, pp.108548 -
Ma, Jinchao (Corresponding author.) , Lu, Yang , Qin, Yifan , Xu, Xice
Abstract Aeroacoustics radiation is one of the main sources of tilt-rotor aircraft interior noise. In order to reduce the noise radiation on the surface of tilt-rotor aircraft fuselage, an active rotor control technology based on Higher Harmonic Control (HHC) is proposed. Its control effect is veri...
Business & Commercial Aviation Leonardo's 46 2020 Bringing tiltrotor technology to civil aviation[J]
Vertiflite Hirschberg 63 6 36 2017 Clean Sky 2 Update, Part 2: The Leonardo Next Generation Civil Tilt rotor[J]
Aerotecnica Missili & Spazio Marano 100 2 111 2021 10.1007/s42496-021-00075-5 Marulo1 Tiltrotor Acoustic Data Acquisition and Analysis
Robert J, Robert A, James C. Noise considerations for tilt-rotor[C]. AIAAIASMEISAEIASEE 25th Joint Propulsion Conference. Monterey, CA I July 10-12, 1989.
Karen HL. XV-15 Structural-acoustic data[R]. NASA Technical Memorandum 112855. 1997.
Fibs J. Stepniewsky WZ. Effect of at-the-source noise reduction on performance and weights of a tilt-rotor aircraft[C]. AIAA 13th Aerospace Sciences Meeting. Pasadena, Calif. January 20-22, 1975.
Khanh N, Mark B, Cahit K. Full-scale demonstration of higher harmonic control for noise and vibration reduction on the XV-15 rotor[C]. American Helicopter Society 56th Annual Forum. Virginia Beach, VA, May 2-4, 2000.
Journal of the American Helicopter Society Edwards 47 4 219 2001 Nasa/Army/Bell XV-15 Tilt-rotor Low-Noise Terminal Area Operations Flight Research Program[J]
Carlos Malpica. Parametric Investigation on the Use of Lateral and Longitudinal Rotor Trim Flapping for Tilt-rotor Noise Reduction[C]. AHS International 73rd Annual Forum & Technology Display, Fort Worth, Texas, USA, May 9-11, 2017.
Journal of Aircraft Gopalan 47 1 41 2010 10.2514/1.35695 Helicopter Thickness Noise Reduction Possibilities Through Active On-Blade Acoustic Control[J]
Chin J Aeronaut Ma 34(11):p.106-118 2021 Experimental Research of Active Cibration and Noise Control of Electrically Controlled Rotor[J]
AIAA Journal Farassat 19 9 1122 1981 10.2514/3.60051 Linear Acoustic Formulas for Calculation of Rotating Blade Noise[J]
Aiaa/ceas Aeroacoustic Conference State College. DLR Kuntz 2013 Rotor Noise Predictions in Hover and Forward Flight Using Different Aeroacoustic Methods[C]
Proceedings of the American Helicopter Society Aeromechanics Specialists’ Meeting Sim 2000 Blade-Vortex Interaction (BVI) Noise: Retreating Side Characteristics[C]. Sensitivity to Chordwise Loading and Unsteady Aerodynamics
10.2514/3.46875 Bagai A, Leishman J G. Rotor Free-Wake Modeling Using a Pseudo-implicit Relaxation Algorithm[J]. Journal of Aircraft, Vol.32, (6), Nov-Dec 1995, pp.1276-1285.
Lamb 1932 Hydrodynamics[M]
Chin J Aeronaut XU 15 1 12 2002 10.1016/S1000-9361(11)60123-4 Prediction of Aerodynamic Interactions of Helicopter Rotor on its Fuselage[J]
Xin J, Li P, Chen R, et al. Theoretical model and experiment on rotor in finite ground effect[J]. Acta Aeronautica et Astronautica Sinica,2017, 38 (3) 120219. (In Chinese)
Vertica Beddoes 7 2 183 1983 Representation of Airfoil Behavior[J]
Kuefmann P, Bartels R, Kessler C, Wall van der B.G. On the Design and Development of a Multiple-Swashplate Control System for the Realization of Individual Blade Control (IBC) for Helicopters[C]. American Helicopter Society 67th Annual Forum, Virginia Beach, VA, May 3-5, 2011.
NASA TM X-62,407. Maid 1975 Tilt-rotor research aircraft familiarization document[R]
Karen HL, Casey L B, Devon SP, A Comparison of Measured and Predicted XV-15 Tilt-rotor Surface Acoustic Pressures[C]. AHS Technical Specialists’ Meeting for Rotorcraft Acoustics and Aerodynamics, Williamsburg, VA, October 28-30, 1997.
Acta Aeronautica et Astronautica Sinica Feng 35 11 2901 2014 Research on the effect of open-loop active blade-pitch control on rotor BVI noise alleviation[J]
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