Experimental and Numerical Analysis of Rotational Speed Influence on the Nonlinear Dynamics of Turbine Blades with Shroud Coupling
Author:
Affiliation:
1. Institute of Dynamics and Vibration Research, Leibniz University Hannover
Publisher
Gas Turbine Society of Japan
Link
https://www.jstage.jst.go.jp/article/jgpp/15/2/15_vol15no2tp03/_pdf
Reference21 articles.
1. Petrov, E. P., 2004, “Method for Direct Parametric Analysis of Nonlinear Forced Response of Bladed DisksWith Friction Contact Interfaces”, Journal of Turbomachinery, Vol. 126, Num. 4., pp. 654-662
2. Szwedowicz, J., Slowik, S., Mahler, A. and Hulme, C.J., 2005, “Nonlinear Dynamic Analyses of a Gas Turbine Blade for Attainment of Reliable Shroud Couplings”, Proceedings of the ASME Turbo Expo 2005: Power for Land, Sea, and Air, ASME
3. Cameron, T.M., Griffin, J.H., Kielb, R.E. and Hoosac, T.M., 1990, “An Integrated Approach for Friction Damper Design”, Journal of Vibration and Acoustics, Vol. 112, Num. 2, pp. 175-182.
4. Griffin, J.H. and Labelle, R.F., 1996, “A Rational Method for Optimizing Shroud Damping”, Proceedings of the ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition, ASME
5. Krack, M., Panning-von Scheidt, L.,Wallaschek, J., Siewert, C. and Hartung, A., 2012, “Robust Design of Friction Interfaces of Bladed Disks With Respect to Parameter Uncertainties”, Proceedings of ASME Turbo Expo 2012, ASME
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