Response of large mistuned bladed disk assembly subjected to random excitations
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/content/pdf/10.1007/s12206-020-0108-5.pdf
Reference20 articles.
1. J. H. Griffin and A. Sinha, The interaction between mistuning and friction in the forced response of bladed disk assemblies, ASME Journal of Engineering for Gas Turbines and Power, 107 (1985) 205–211.
2. A. Sinha, Friction damping of random vibration in gas turbine engine airfoils, International Journal of Turbo and Jet Engines, 7 (1990) 95–102.
3. C.-C. Lin and M. P. Mignolet, An adaptive perturbation scheme for the analysis of mistuned bladed disks, ASME Journal of Engineering for Gas Turbines and Power, 119 (1997) 153–160.
4. D. S. Whitehead, The maximum factor by which forced vibration of blades can increase due to mistuning, ASME Journal of Engineering for Gas Turbines and Power, 120 (1998) 115–119.
5. D. Cha and A. Sinha, Statistics of response of a mistuned bladed disk assembly subjected to white noise and narrow band excitation, ASME Journal of Engineering for Gas Turbines and Power, 121 (1999) 710–717.
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