Flutter analysis of mistuned bladed disk-Reference-Cited by-同舟云学术

Flutter analysis of mistuned bladed disk

Published:2015 Issue:824 Volume:81 Page:14-00491-14-00491
ISSN:2187-9761
Container-title:Transactions of the JSME (in Japanese)
language:en
Short-container-title:

Author:

KANEKO Yasutomo¹,TAKEMURA Makoto¹,MORI Kazushi²,OOYAMA Hiroharu³

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/81/824/81_14-00491/_pdf

Reference11 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., Vibration 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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