This paper presents important improvements and extensions to a computationally efficient reduced order modeling technique for the vibration analysis of mistuned bladed disks. In particular, this work shows how the existing modeling technique is readily extended to turbomachinery rotors with shrouded blades. The modeling technique employs a component mode synthesis approach to systematically generate a Reduced Order Model (ROM) using component modes calculated from a Finite Element Model (FEM) of the rotor. Based on the total number of degrees of freedom, the ROM is typically two or three orders of magnitude smaller than the FEM. This makes it feasible to predict the forced response statistics of mistuned bladed disks using Monte Carlo simulations. In this work, particular attention is devoted to the introduction of mistuning into the ROM of a shrouded assembly. Mistuning is modeled by projecting the mistuned natural frequencies of a single, cantilever blade with free shrouds onto the harmonic modes of the shrouded blade assembly. Thus, the necessary mistuning information may be measured by testing individual blades.
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ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition
June 2–5, 1998
Stockholm, Sweden
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7866-8
PROCEEDINGS PAPER
Reduced Order Modeling and Vibration Analysis of Mistuned Bladed Disk Assemblies With Shrouds
Ronnie Bladh,
Ronnie Bladh
The University of Michigan, Ann Arbor, MI
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Matthew P. Castanier,
Matthew P. Castanier
The University of Michigan, Ann Arbor, MI
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Christophe Pierre
Christophe Pierre
The University of Michigan, Ann Arbor, MI
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Ronnie Bladh
The University of Michigan, Ann Arbor, MI
Matthew P. Castanier
The University of Michigan, Ann Arbor, MI
Christophe Pierre
The University of Michigan, Ann Arbor, MI
Paper No:
98-GT-484, V005T14A041; 10 pages
Published Online:
December 23, 2014
Citation
Bladh, R, Castanier, MP, & Pierre, C. "Reduced Order Modeling and Vibration Analysis of Mistuned Bladed Disk Assemblies With Shrouds." Proceedings of the ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition. Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education. Stockholm, Sweden. June 2–5, 1998. V005T14A041. ASME. https://doi.org/10.1115/98-GT-484
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