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    Analysis of the Effect of Multirow and Multipassage Aerodynamic Interaction on the Forced Response Variation in a Compressor Configuration—Part I: Aerodynamic Excitation 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 005:;page 51004
    Author(s): Schoenenborn, Harald
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aeroelastic prediction of blade forcing is still a very important topic in turbomachinery design. Usually, the wake from an upstream airfoil and the potential field from a downstream airfoil are considered as the main ...
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    Aeroelasticity at Reversed Flow Conditions—Part III: Reduction of Surge Loads by Means of Intentional Mistuning 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 004:;page 41009
    Author(s): Schoenenborn, Harald; de Vries, Mirja
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Compressor surge consists of four phases: (i) pressure rise, (ii) flow breakdown, (iii) blowdown, and (iv) flow recovery. During the blowdown phase reversed flow conditions exist, where a blade may accumulate hundreds of ...
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    Analysis of the Effect of Multirow and Multipassage Aerodynamic Interaction on the Forced Response Variation in a Compressor Configuration—Part II: Effects of Additional Structural Mistuning 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 005:;page 51005
    Author(s): Gross, Johann; Krack, Malte; Schoenenborn, Harald
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The prediction of aerodynamic blade forcing is a very important topic in turbomachinery design. Usually, the wake from the upstream blade row and the potential field from the downstream blade row are considered as the main ...
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    Identification of Mistuning Based on Forced Response Measurements and Assessment for a Real Compressor Blisk 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 009:;page 91006
    Author(s): Seeger, Benjamin;Kohlmann, Lukas;Schoenenborn, Harald;Schwarz, Stefan;Krack, Malte
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: We develop a novel method for the identification of mistuned blisks. The method relies on forced response measurements in a certain target frequency band. Modal stiffness deviations and an overall structural damping ...
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