Volume 27 Issue 4
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SHA Hong-wei, CHEN Ren-liang. Flight dynamics characteristic of tilt rotor aircraft[J]. Journal of Aerospace Power, 2012, 27(4): 749-754.
Citation: SHA Hong-wei, CHEN Ren-liang. Flight dynamics characteristic of tilt rotor aircraft[J]. Journal of Aerospace Power, 2012, 27(4): 749-754.
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Flight dynamics characteristic of tilt rotor aircraft

  • National Key Laboratory of Rotorcraft Aeromechanics, College of Aeronautics and Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

  • Received Date: 2011-01-28
  • Rev Recd Date: 2012-02-09
  • Publish Date: 2012-04-28
    Abstract
  • A flight dynamics model of the tilt rotor aircraft was established based on the research into the aerodynamic of the rotors,wing,fuselage,nacelle,empennage and control system.Quasi-steady element theory was used to analyze the lift,drag,moment and the flapping motion of the rotors.The lift line theory was used to research the aerodynamics of others,and then an investigation was conducted on the XV-15 tilt rotor aircraft.The results can be helpful to realize the characteristics of tilt rotor aircraft,also be useful to flight control design.

     

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    • References(12)
  • [1]
    Harendra P B,Joglekar M J,Gaffey T M,et al.A mathematical model for real time flight simulation of the Bell Model 301 tilt rotor research aircraft.NASA-CR-114614,1973.
    [2]
    Martin D,Maisel,Demo J,et al.The histroy of the XV-15 tilt rotor research aircraft.NASA SP-2000-4517,2000.
    [3]
    Menger R P,Hogg C B.Recent investigation in tilt rotor flight technology through XV-15 flight testing //Proceedings of American Helicopter Society 43rd Annual Forum.St.Louis,MO:American Helicopter Society,1987:18-20.
    [4]
    沙虹伟.无人倾转旋翼机飞行力学建模与姿态控制技术研究.南京:南京航空航天大学,2007. SHA Hongwei.A mathematical model of unmanned tiltrotor aircraft and research on attitude control system design.Nanjing:Nanjing University of Aeronautics and Astronautics 2007.(in Chinese)
    [5]
    Chen R T N.Effects of primary rotor parameters on flapping dynamics.NASA TM-431,1980.
    [6]
    Chen R TN.A simplified rotor system mathematical model for piloted flight dynamics simulation.NASA TM-78575,1973.
    [7]
    Carlson E B,ZHAO Yiyuan,Robert T N.Optimal tiltrotor runway operations in one engine inoperative.AIAA-99-3961,1999.
    [8]
    Gill P E,Murray W,Saunders M A,et al.User’s guide for snopt version 6,a fortran package for nonlinear programming.California 94305-4026,2002.
    [9]
    Gill P E,Murray W,Saunders M A.An SQP algorithm for large-scale constrained optimization[J].Society for industrial and applied mathematics,2005,47(1):99-131.
    [10]
    Kristi M K.Stability and control modeling of tilt-rotor aircraft.Maryland:University of Maryland,2007.
    [11]
    Ferguson,Samuel W A.Mathematical model for real time flight simulation of a generic tilt-prop rotor aircraft.NASA-CR-166536,1983.
    [12]
    宋彦国,王焕瑾,沙虹伟,等,倾转旋翼飞行器飞行力学模型研究[J].空气动力学学报,2008,26(2):192-196. SONG Yanguo,WANG Huanjin,SHA Hongwei,et al.Flight dynamic mathematical model of tiltrotor aircraft[J].Acta Aerodynamica Sinica,2008,26(2):192-196.(in Chinese)
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