CHEN Heng, WANG Yang-yu, JIN Jiang-ming. Flutter Characteristics Analysis of 2D Rigid Airfoils With Control Surface Based on the Arc-Length Numerical Continuation Method[J]. Applied Mathematics and Mechanics, 2017, 38(7): 769-779. doi: 10.21656/1000-0887.370223
Citation: CHEN Heng, WANG Yang-yu, JIN Jiang-ming. Flutter Characteristics Analysis of 2D Rigid Airfoils With Control Surface Based on the Arc-Length Numerical Continuation Method[J]. Applied Mathematics and Mechanics, 2017, 38(7): 769-779. doi: 10.21656/1000-0887.370223

Flutter Characteristics Analysis of 2D Rigid Airfoils With Control Surface Based on the Arc-Length Numerical Continuation Method

doi: 10.21656/1000-0887.370223
Funds:  The National Natural Science Foundation of China(51405440)
  • Received Date: 2016-07-21
  • Rev Recd Date: 2016-09-13
  • Publish Date: 2017-07-15
  • A 3-DOF aeroelastic model was built for 2D rigid airfoils with control surface. This model was simplified with cubic nonlinear stiffness in heave and pitch, where the freeplay control surface was replaced with bilinear stiffness. According to the quasi-steady aerodynamic theory, the motion equations for the system was established. The peak-to-peak value diagram was used to depict the global dynamic properties of the airfoil at different flow velocities, and the arc-length numerical continuation method together with the Floquet multiplier was applied to construct the bifurcation diagram and study the aerodynamic stability. The bifurcation diagram matched the peak-to-peak value diagram well. The results show there are various dynamic behaviors due to freeplay nonlinearity. The aeroelastic model yields complicated limit cycle oscillations, quasi-periodic motions and chaotic phenomena when the angular displacement of the control surface reaches the clearance limit.
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  • [1]
    Bunton R W, Denegri C W. Limit cycle oscillation characteristics of fighter aircraft[J]. Journal of Aircraft, Engineering Note,2000,37(5): 916-918.
    [2]
    Gilliatt H C, Strganac T W, Kurdila A J. Nonlinear aeroelastic response of an airfoil[C]//35th AIAA Aerospace Sciences Meeting and Exhibit . Reno, NV, USA, 1997: AIAA Paper 97-0459.
    [3]
    Jones D P, Roberts I, Gaitonde A L. Identification of limit cycles for piecewise nonlinear aeroelastic systems[J]. Journal of Fluids and Structures,2007,23(7): 1012-1028.
    [4]
    TANG De-man, Dowell E H. Experimental and theoretical study of gust response for a wing-store model with freeplay[J]. Journal of Sound and Vibration,2006,295(3/5): 659-684.
    [5]
    郭虎伦, 陈予恕. 超声速流中含间隙和立方非线性二元机翼的动力学分析[J]. 应用数学和力学, 2012,33(1): 1-13.(GUO Hu-lun, CHEN Yu-shu. Dynamic analysis of a two-degree-of-freedom airfoil with freeplay and cubic nonlinearities in supersonic flow[J]. Applied Mathematics and Mechanics,2012,33(1): 1-13.(in Chinese))
    [6]
    齐欢欢, 徐鉴, 方明霞. 超音速飞行器机翼颤振的时滞反馈控制[J]. 应用数学和力学, 2016,〖STHZ〗37(2): 210-218. (QI Huan-huan, XU Jian, FANG Ming-xia. Time-delayed feedback control of flutter for supersonic airfoils[J]. Applied Mathematics and Mechanics,2016,37(2): 210-218.(in Chinese))
    [7]
    赵永辉, 胡海岩. 大展弦比夹芯翼大攻角颤振分析[J]. 振动工程学报, 2004,17(1): 25-30.(ZHAO Yong-hui, HU Hai-yan. Flutter analysis of a high-aspect-ratio sandwich wing under large angle of attack[J]. Journal of Vibration Engineering,2004,17(1): 25-30. (in Chinese))
    [8]
    崔鹏, 韩景龙. 新型运输机机翼的颤振特性分析[J]. 振动工程学报, 2011,24(2): 192-199.(CUI Peng, HAN Jing-long. Flutter analysis of new transport-type wings[J]. Journal of Vibration Engineering,2011,24(2): 192-199.(in Chinese))
    [9]
    周秋萍, 邱志平. 机翼带外挂系统极限环颤振的区间分析[J]. 航空学报, 2010,31(3): 514-518.(ZHOU Qiu-ping, QIU Zhi-ping. Interval analysis for limit cycle flutter of a wing with an external store[J]. Acta Aeronautica et Astronautica Sinica,2010,31(3): 514-518.(in Chinese))
    [10]
    史爱明, 杨永年, 叶正寅. 带结构刚度非线性的超音速弹翼颤振分析方法研究[J]. 西北工业大学学报, 2003,21(4): 481-485.(SHI Ai-ming, YANG Yong-nian, YE Zheng-yin. Investigation of flutter characteristics of wing with nonlinear stiffness in supersonic flow[J]. Journal of Northwestern Polytechnical University,2003,21(4): 481-485.(in Chinese))
    [11]
    Vio G A, Cooper J E. Limit cycle oscillation prediction for aeroelastic systems with discrete bilinear stiffness[J]. International Journal of Applied Mathematics and Mechanics,2005,3: 100-119.
    [12]
    Liu L, Wong Y S, Lee B H K. Application of the centre manifold theory in non-linear aeroelasticity[J]. Journal of Sound and Vibration,2000,234(4): 641-659.
    [13]
    Levitas J, Weller T, Singer J. Poincaré-like simple cell mapping for non-linear dynamical systems[J]. Journal of Sound and Vibration,1994,176(5): 641-662.
    [14]
    Raghothama A, Narayanan S. Non-linear dynamics of a two-dimensional airfoil by incremental harmonic balance method[J]. Journal of Sound and Vibration,1999,226(3): 493-517.
    [15]
    Dimitriadis G. Bifurcation analysis of aircraft with structural nonlinearity and freeplay using numerical continuation[J]. Journal of Aircraft,2008,45(3): 893-905.
    [16]
    Kubicek M. Algorithm 502: dependence of solution of nonlinear systems on a parameter[J]. ACM Transactions on Mathematical Software,1976,2(1): 98-107.
    [17]
    Doedel E J, Champneys A R, Fairgrieve T F, et al. AUTO97-AUTO2000: continuation and bifurcation software for ordinary differential equations (with HomCont): user’s guide, tech rept[R]. Montreal, Canada: Concordia University, 2000.
    [18]
    Dhooge A, Govaerts W, Kuznetsov Y A. MATCONT: a MATLAB package for numerical bifurcation of ODEs[J]. ACM Transactions on Mathematical Software,2003,29(2): 141-164.
    [19]
    Roberts I, Jones D P, Lieven N A J, et al. Analysis of piecewise linear aeroe-lastic systems using numerical continuation[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2002,216(1): 1-11.
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