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    Convective Heat Transfer and Aerodynamics in Axial Flow Turbines 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 004:;page 637
    Author(s): Michael G. Dunn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The primary focus of this paper is convective heat transfer in axial flow turbines. Research activity involving heat transfer generally separates into two related areas: predictions and measurements. ...
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    Heat-Transfer Measurements and Predictions for the Vane and Blade of a Rotating High-Pressure Turbine Stage 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 001:;page 101
    Author(s): Charles W. Haldeman; Michael G. Dunn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes heat-transfer measurements and predictions obtained for the vane and blade of a rotating high-pressure turbine stage. The measurements were obtained with the stage operating ...
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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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    Relationship Between Mechanical Properties and Collagen Structure of Closed and Open Wounds 

    Source: Journal of Biomechanical Engineering:;1988:;volume( 110 ):;issue: 004:;page 352
    Author(s): Charles J. Doillon; Michael G. Dunn; Frederick H. Silver
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Mechanical properties and collagen structure of excisional wounds left open are compared with wounds closed by clips. In both wound models, collagen fiber diameter increases with time post-wounding ...
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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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    Temperature Predictions and Comparison With Measurements for the Blade Leading Edge and Platform of a 1 1/2 Stage Transonic HP Turbine 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 001:;page 11016
    Author(s): Randall M. Mathison; Mark B. Wishart; Charles W. Haldeman; Michael G. Dunn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A series of computational predictions generated using FINE/TURBO are compared with data to investigate implementation techniques available for predicting temperature migration through a turbine ...
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    Investigation of Turbine Shroud Distortions on the Aerodynamics of a One and One-Half Stage High-Pressure Turbine 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 003:;page 31002
    Author(s): Eric A. Crosh; D. Graham Holmes; Brian E. Mitchell; Charles W. Haldeman; Michael G. Dunn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As part of a proactive effort to investigate the ability of computational fluid dynamics tools to predict time-accurate surface-pressure histories, a combined experimental/computational investigation ...
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    Averaged and Time-Dependent Aerodynamics of a High Pressure Turbine Blade Tip Cavity and Stationary Shroud: Comparison of Computational and Experimental Results 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 004:;page 736
    Author(s): Brian R. Green; Charles W. Haldeman; Michael G. Dunn; John W. Barter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady aero-dynamics of a single-stage high-pressure turbine blade operating at design corrected conditions has been the subject of a thorough study involving detailed measurements and ...
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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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    Aerodynamic and Heat-flux Measurements with Predictions on a Modern One and One-Half State High Pressure transonic Turbine 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 003:;page 522
    Author(s): Charles W. Haldeman; John W. Barter; Brain R. Green; Michael G. Dunn; Robert F. Bergholz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Aerodynamic and heat-transfer measurements were acquired using a modern stage and 1∕2 high-pressure turbine operating at design corrected conditions and pressure ratio. These measurements were ...
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