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    Reduced Order Modeling and Vibration Analysis of Mistuned Bladed Disk Assemblies With Shrouds 

    Source: Journal of Engineering for Gas Turbines and Power:;1999:;volume( 121 ):;issue: 003:;page 515
    Author(s): R. Bladh; M. P. Castanier; C. Pierre
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: 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 ...
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    Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks—Part II: Application 

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 001:;page 100
    Author(s): R. Bladh; M. P. Castanier; Assistant Research Scientist; C. Pierre
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the component-mode-based methods formulated in the companion paper (Part I: Theoretical Models) are applied to the dynamic analysis of two example finite element models of bladed ...
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    Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks—Part I: Theoretical Models 

    Source: Journal of Engineering for Gas Turbines and Power:;2001:;volume( 123 ):;issue: 001:;page 89
    Author(s): R. Bladh; M. P. Castanier; Assistant Research Scientist; C. Pierre
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Component mode synthesis (CMS) techniques are widely used for dynamic analyses of complex structures. Significant computational savings can be achieved by using CMS, since a modal analysis is ...
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    Effects of Multistage Coupling and Disk Flexibility on Mistuned Bladed Disk Dynamics 

    Source: Journal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 001:;page 121
    Author(s): R. Bladh; M. P. Castanier; Assistant Research Scientist; C. Pierre
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of disk flexibility and multistage coupling on the dynamics of bladed disks with and without blade mistuning are investigated. Both free and forced responses are examined using ...
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    Dynamic Response Predictions for a Mistuned Industrial Turbomachinery Rotor Using Reduced-Order Modeling 

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 002:;page 311
    Author(s): R. Bladh; M. P. Castanier; Assistant Research Scientist; M. J. Kruse; Senior Engineer; C. Pierre
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper explores the effects of random blade mistuning on the dynamics of an advanced industrial compressor rotor, using a component-mode-based reduced-order model formulation for tuned and ...
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