Reduced Order Modeling of a Bladed Rotor with Geometric Mistuning: Alternative Bases and Extremely Large Mistuning
Author:
Affiliation:
1. Sr. Software Developer, ANSYS, Inc.
2. Department of Mechanical & Nuclear Engineering, The Pennsylvania State University
Publisher
Gas Turbine Society of Japan
Subject
Mechanical Engineering
Link
https://www.jstage.jst.go.jp/article/jgpp/5/1/5_1/_pdf
Reference11 articles.
1. Bhartiya, Y. and Sinha, A., “Reduced Order Model of a Bladed Rotor with Geometric Mistuning: Comparison Between Modified Modal Domain Analysis and Frequency Mistuning Approach,” GT2011-45391, presented at the ASME Turbo Expo, Vancouver, BC, Canada, June 6 – 11, 2011.
2. Bhartiya, Y. and Sinha, A., “Reduced Order Modeling of a Bladed Rotor with Geometric Mistuning via Estimated Deviations in Mass and Stiffness Matrices,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 135, No. 5, May 2013. (Also, DETC 2011-47495).
3. Brown, J. M., ”Reduced Order Modeling Methods for Turbomachinery Design”, Ph.D. dissertation, Wright State University, Dayton, Ohio, 2008.
4. Ganine, V., Legrand, M., Michalska, H., and Pierre, C. , “ A Sparse Preconditioned Iterative Method for Vibration Analysis of Geometrically Mistuned Bladed Disks,” Computers and Structures, Vol. 87, 2009, pp. 342 – 354.
5. Ghanem, R.G., and Spanos, P.D., Stochastic Finite Elements: A Spectral Approach, Springer, New York, 1991
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1. Reduced Order Models for Largely Mistuned Blisks with Small Random Mistuning;AIAA Journal;2020-06
2. Response of large mistuned bladed disk assembly subjected to random excitations;Journal of Mechanical Science and Technology;2020-02
3. Forced Response Statistics of a Bladed Rotor with Geometric Mistuning;AIAA Journal;2015-09
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