Study on optimal design of mistuned bladed disk
Author:
Affiliation:
1. Department of Mechanical and Systems Engineering, Ryukoku University
2. Mitsubishi Heavy Industries, Ltd.
3. Mitsubishi Hitachi Power Systems, Ltd.
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/transjsme/84/861/84_17-00447/_pdf
Reference13 articles.
1. Bendiksen, O. O., Flutter of mistuned turbomachinery rotor, ASME Journal of Engineering for Gas Turbines and Power, No. 106 (1984),pp.25-33.
2. Carlos, M., Roque, C. and Jose, M. L., Stability increase of aerodynamically unstable rotors using intentional mistuning, ASME Journal of Turbomachinery, Vol. 130, 011006 (2008), pp.1-10.
3. Feiner, D. M. and Griffin, J. H., A fundamental model of mistuning for a single family of modes, ASME, Journal of Turbomachinery, Vol.124 (2002), pp.597-605.
4. Feiner, D. M. and Griffin, J. H., Mistuning identification of bladed disks using a fundamental mistuning model-part 1: theory, Proceedings of ASME Turbo Expo 2003, GT2003-38952 (2003), pp.1-10.
5. Kaneko, Y., Mase, M., Fujita, K. and Nagashima, T., Vibrational response analysis of mistuned bladed disk, Transactions of the Japan Society of Mechanical Engineers, Series C, Vol.58, No.547 (1992), pp.744-749 (in Japanese).
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