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    Airfoil Deflection Characteristics During Rub Events 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 001:;page 11018
    Author(s): Kevin E. Turner; Michael Dunn; Corso Padova
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The turbomachinery industry continually struggles with the adverse effects of contact rubs between airfoils and casings. The key parameter controlling the severity of a given rub event is the ...
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    Experimental Results From Controlled Blade Tip/Shroud Rubs at Engine Speed 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 004:;page 713
    Author(s): Corso Padova; Steve Manwaring; Jeffery Barton; Michael G. Dunn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results obtained for an Inconel® compressor blade rubbing a steel casing at engine speed are described. Load cell, strain gauge, and accelerometer measurements are discussed and ...
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    Casing Treatment and Blade-Tip Configuration Effects on Controlled Gas Turbine Blade Tip/Shroud Rubs at Engine Conditions 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001:;page 11016
    Author(s): Corso Padova; Kevin Turner; Alan Turner; Michael G. Dunn; Jeffery Barton; Darin DiTommaso
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results obtained for an Inconel® compressor blade rubbing bare-steel and treated casings at engine speed are described. Since 2002 a number of experiments were conducted to ...
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    Development of an Experimental Capability to Produce Controlled Blade Tip∕Shroud Rubs at Engine Speed 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 004:;page 726
    Author(s): Corso Padova; Steve Manwaring; Maurice Adams; Michael Adams; Gamaliel Young; Jeffrey Barton; Michael G. Dunn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental capability using an in-ground spin-pit facility specifically designed to investigate aeromechanic phenomena for gas turbine engine hardware rotating at engine speed is demonstrated ...
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