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    Transient Forced Response Analysis of Mistuned Steam Turbine Blades During Startup and Coastdown 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 001:;page 12501
    Author(s): Siewert, Christian; Stüer, Heinrich
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is well known that the vibrational behavior of a mistuned bladed disk differs strongly from that of a tuned bladed disk. A large number of publications dealing with the dynamics of mistuned bladed disks are available ...
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    Reduced Order Modeling Based on Complex Nonlinear Modal Analysis and Its Application to Bladed Disks With Shroud Contact 

    Source: Journal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 010:;page 102502
    Author(s): Krack, Malte; Panning; Wallaschek, Jأ¶rg; Siewert, Christian; Hartung, Andreas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design of bladed disks with contact interfaces typically requires analyses of the resonant forced response and flutterinduced limit cycle oscillations. The steadystate vibration behavior can efficiently be calculated ...
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    Detection of Cracks in Turbomachinery Blades by Online Monitoring 

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 145 ):;issue: 004:;page 41023-1
    Author(s): Kumar, Manish; Heinig, Roger; Cottrell, Mark; Siewert, Christian; Almstedt, Henning; Feiner, Drew; Griffin, Jerry
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The presence of a crack in a blade can change the natural frequencies of that blade. It has long been a goal to detect blade cracks by assessing the change in a measured vibration frequency of the blade over time. It has ...
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