Optics and Precision Engineering, Volume. 25, Issue 5, 1259(2017)

Drag-reduction inverse design of wings based on lifting-line theory

JIANG Yue-ning1...2,* and JIA Hong-guang13 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    References(17)

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    [3] [3] TANG D M, DOWELL E H. Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings [J]. AIAA Journal, 2001, 39(8): 1430-1441.

    [4] [4] SI L, WANG H P, GONG C C. Investigation of effects of winglets on wings aerodynamic and structural behavior [J].Acta Aerodynamica Sinica, 2011, 29(2): 177-181. (in Chinese)

    [5] [5] LI F W. Introduction of Air and Gas Dynamics [M]. Xian: Northwestern Polytechnical University Press, 2007: 129-132. (in Chinese)

    [6] [6] EDITORIAL BOARD OF AIRCRAFT DESIGN HANDBOOK. Aircraft Design Handbook Vol.6: Aerodynamic Design [M]. Beijing: Aviation Industry Press, 2002.(in Chinese)

    [7] [7] PHILLIPS W F. Lifting-line analysis for twisted wings and washout-optimized wings [J]. Journal of Aircraft, 2004, 41(1): 128-136.

    [10] [10] WANG X P. Optimization and design for aerodynamic configuration of aircraft based on genetic algorithm [J]. Chinese Journal of Computational Mechanics, 2002, 19(2): 188-201.(in Chinese)

    [11] [11] LI Y, ZHU Z Q, WANG X L, et al.. Optimization design of wings thickness and twist angle using Euler equations [J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(3): 269-272, 277. (in Chinese)

    [12] [12] TAKAHASHI T T, COOPERSMITH R M. Wing section design for a long-range hydrofoil transport [C]. AIAA, 2002.

    [13] [13] RASMUSSEN M L, SMITH D E. Lifting-line theory for arbitrarily shaped wings [J]. Journal of Aircraft, 1999, 36(2): 340-348.

    [14] [14] LI J Z, GAO ZH H, ZHAN H. Study on inverse design method of airfoil based on optimization of target pressure distribution [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2008, 28(1): 187-190.(in Chinese)

    [15] [15] YANG X D, QIAO ZH D, ZHU B.Wing design method and application based on Euler equations [J]. Acta Acrodynamica Sinica, 2001, 19(1): 97-102. (in Chinese)

    [16] [16] QIAO Y H, MA D L, DENG X G. Wing geometric twist design method based on lifting-line theory [J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(3): 320-324. (in Chinese)

    [17] [17] SCHMITT V, CHARPIN F. Pressure distributions on the ONERA-M6 wing at transonic mach numbers [R]. AGARD-AR-138, 1979.

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    JIANG Yue-ning, JIA Hong-guang. Drag-reduction inverse design of wings based on lifting-line theory[J]. Optics and Precision Engineering, 2017, 25(5): 1259

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    Paper Information

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    Received: Jun. 23, 2016

    Accepted: --

    Published Online: Jun. 30, 2017

    The Author Email: Yue-ning JIANG (atpynjiang@163.com)

    DOI:10.3788/ope.20172505.1259

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