Volume 36 Issue 2
Feb.  2010
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Wu Zhigang, Song Chen, Yang Chaoet al. Mode tracking techniques in flutter analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(2): 163-167. (in Chinese)
Citation: Wu Zhigang, Song Chen, Yang Chaoet al. Mode tracking techniques in flutter analysis[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(2): 163-167. (in Chinese)

Mode tracking techniques in flutter analysis

  • Received Date: 20 Feb 2009
  • Publish Date: 28 Feb 2010
  • Flutter solution is an eigenvalue problem which has variable parameters (such as air speed). In flutter mode identification and flutter prevention, the correspondence between the baseline and perturbed eigenvalues due to parameter variation should be determined accurately, and mode crossing should be avoided. For mode tracking in flutter solution p-k/i> procedure, the forecast tracking method was developed, which was based on the perturbation theory of eigenvalues. The method used the baseline eigenvalues and the left and right eigenvectors to estimate perturbed eigenvalues, and sorted modes by their estimated values. The forecast tracking method was compared with two existing methods, one was similarity sorting method, the other was orthogonality check method. Two testing cases were used to validate the effectiveness of the methods. The numerical results show that the forecast tracking method is better than the existing methods in effects of mode tracking.

     

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  • [1] 管德.飞机气动弹性力学手册[M].北京:航空工业出版社,1994:126-134 Guan De. Aeroelasticity handbook of aircraft[M].Beijing: Aeronautical Industry Press,1994:126-134(in Chinese) [2] 谢长川,胡薇薇,杨超.颤振分析中的特征值排序问题[J].数学的实践与认识,2007,37(18):141-146 Xie Changchuan,Hu Weiwei,Yang Chao.Eigenvalue sorting problem in flutter analysis[J].Mathematics in Practice and Theory,2007,37(18):141-146(in Chinese) [3] Desmarais R N,Bennett R M.An automated procedure for computing flutter eigenvalues[J].Journal of Aircraft,1974,11(2):75-80 [4] Van Zyl L H.Use of eigenvectors in the solution of the flutter equation[J].Journal of Aircraft,1993,30(4):553-554 [5] Eldred M S,Venkayya V B,Anderson W J.New mode tracking methods in aeroelastic analysis[J].AIAA Journal,1995,33(7):1292-1299 [6] Chen P C.A damping perturbation method for flutter solution:the g-method[J].AIAA Journal,2000,38(9):1519-1524 [7] ZONA Techonology Inc.ZAERO version7.4 theoretical manual[M].Scottsdale:ZONA Techonology Inc,2006:7-8-7-12 [8] Hassig H J.An approximate true damping solution of the flutter equation by determinant iteration[J].Journal of Aircraft,1971,8(11):885-889 [9] Rodden W P,Johnson E H.MSC/NASTRAN v68 aeroelastic analysis user-s guide[M].Los Angeles:MacNeal-Schwendler Corp,1994:97-101 [10] Karpel M.Sensitivity derivatives of flutter characteristics and stability margins for aeroservoelastic design[J].Journal of Aircraft,1990,27(4):368-375
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