یافتن بدترین پاسخ فرکانسی سیستم دیسک پره دار تحت تاثیر نامیزانی به کمک الگوریتم ژنتیک

[1] J.H. Griffin, A. Sinha, “The interaction between mistuning and friction in the forced response of bladed disk assemblies”, Journal of Engineering for Gas Turbines and Power, Vol. 107, pp. 205–211, 1985.

[2] D.S. Whitehead, “Effects of mistuning on the vibration of turbomachinary blades induced by wakes”, J.Mechanical Engineering Science, Vol.8, No. 1, pp. 15–21, 1966.

[3] D.S. Whitehead, “Effects of Mistuning on Forced Vibration of Blades with Mechanical Coupling”, Journal of Mechanical Engineering Science, Vol.18, No. 6, pp.306-307, 1976.

[4] R.C.F. Dye, T.A. Henry, “Vibration amplitudes of compressor blades resulting from scatter in blade natural

frequencies”, ASME, Journal of Engineering for Power,Vol. 91, No. 3, pp. 182-188, 1969.

[5] Wagner, J.T., “Coupling of turbomachine blade vibrations through the rotor”, ASME, Journal of Engineering for Power, Vol. 89, No. 4, pp. 502–512,1967.

[6] D.J. Ewins, “The effect of detuning upon the forced vibration of bladed disks”, J. Sound and Vibration,Vol.9, pp. 65–79, 1969.

[7] L.E. EL-Bayoumy, A.E. Srinivasan, “Influence of mistuning on rotor blade vibration, AIAA Journal, Vol.13, No. 4, pp. 460–464, 1975.

[8] Afolabi, D.H., Vibration of Mistuned Bladed Disc Assembly, PhD Thesis, Imperial College of Science, Technology & Medicines, University of London, 1982.

[9] Afolabi, D.H. “Vibration Amplitudes of Mistuned Blades”, ASME, Journal of Turbomachinary, Vol. 110,pp. 251–257, 1988.

[10] Lin C.C., Mignolet M.P., “Effects of Damping and Damping Mistuning on the Forced Vibration Response of Bladed Disks”, J. Sound Vib. Vol. 193, pp. 525-543,1996.

[11] Y.J. Chiu, Sh.Ch. Huang, “The influence on coupling vibration of a rotor system due to a mistuned blade length”, Journal of Mechanical Sciences, Vol. 49, pp.522–532, 2007.

[12] Y.J. Yan, P.L. Cui, H.N. Hao, “Vibration mechanism of a mistuned bladed-disk”, Journal of Sound and Vibration, Vol. 317, pp. 294–307, 2008.

[13] Y.-J. Chan , D.J. Ewins, “Management of the variability of vibration response levels in mistuned bladed discs using robust design concepts. Part 1 Parameter design”,J. Mechanical Systems and Signal Processing, Vol. 24,pp. 2777–2791, 2010.

[14] J.H. Griffin, A. Sinha, “The interaction between mistuning and friction in the forced response of bladed disk assemblies”, Journal of Engineering for Gas Turbines and Power, Vol. 107, pp. 205–211, 1985.

[15] J.H. Griffin, “On predicting the resonant response of bladed disk assemblies”, Journal of Engineering for Gas Turbines and Power, Vol. 110, pp. 45–50, 1988.

[16] R.L. Jay, D.W. Burns, “Characteristics of the diametral resonant response of a shrouded fan under a prescribed distortion”, Journal of Vibration, Acoustics, Stress and Reliability in Design, Vol. 108, pp. 125–131, 1986.

[17] A. Sinha, S. Chen, “A higher order technique to compute the statistics of forced response of a mistuned bladed disk”, Journal of Sound and Vibration, Vol. 130, pp. 207–221, 1989.

[18] A. Sinha, “Calculating the statistics of forced response of a mistuned bladed disk assembly”, American Institute of Aeronautics and Astronautics Journal, Vol. 24, pp. 1797–1801, 1986.

[19] M.P. Mignolet, C.C. Lin, “The combined closed form-perturbation approach to the analysis of mistuned bladed disks”, Journal of Turbomachinery, Vol. 115, pp. 771–780, 1993.

[20] C.C. Lin, The combined closed form-perturbation approach to the analysis of mistuned bladed disks,M.S. Thesis, Arizona State University, 1991.

[21] Goldberg, D. E., Genetic Algorithms in Search,Optimization, and Machine Learning, Addison-Weslcy,Reading, MA, 1989.

[22] Davis (Ed.), L., Handbook of Genetic Algorithms, Van Nostrand Reinhold, 1991.