Study on identification of modal parameters of mistuned bladed disks (Identification by use of the frequency response curve and the reduced order model)
Author:
Affiliation:
1. Department of Mechanical and Systems Engineering, Ryukoku University
2. Mitsubishi Heavy Industries, Ltd.
Publisher
Japan Society of Mechanical Engineers
Subject
General Medicine
Link
https://www.jstage.jst.go.jp/article/transjsme/89/924/89_22-00286/_pdf
Reference13 articles.
1. Feiner, D. M. and Griffin, J. H., A fundamental model of mistuning for a single family of modes, Transactions of the ASME, Journal of Turbomachinery, Vol.124 (2002), pp.597-605.
2. Feiner, D. M. and Griffin, J. H., Mistuning identification of bladed disks using a fundamental Mistuning Model−Part 1: Theory, Transactions of ASME, Journal of Turbomachinery, Vol.126 (2004), pp.150-158.
3. Figaschewsky, F. and Kühhorn, A., An inverse approach to identify tuned aerodynamic damping, system frequencies and mistuning. Part 1: Theory and benchmark under rotating conditions, Proceedings of the 15th ISUAAAT, Paper No. ISUAAAT15-048 (2018), pp.1-13.
4. Kaneko, Y., Mechanical design of gas turbine blade, Journal of the Gas Turbine Society of Japan, Vol. 133, No. 1 (2005), pp.4-111 (in Japanese).
5. Kaneko, Y., Iiduka, S. and Ikegami, Y., Development of non-contact measurement method of turbomachinery blade vibration (Improved few-probe method), Transactions of the Japan Society of Mechanical Engineers, Series C, Vol. 67, No. 658 (2001), pp.1846–1852 (in Japanese).
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