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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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    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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    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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    Experimental Investigation of Vane Clocking in a One and One-Half Stage High Pressure Turbine 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 003:;page 512
    Author(s): Charles W. Haldeman; John W. Barter; Brian R. Green; Michael Dunn; Robert F. Bergholz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Aerodynamic measurements were acquired on a modern single-stage, transonic, high-pressure turbine with the adjacent low-pressure turbine vane row (a typical civilian one and one-half stage turbine ...
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    Heat Transfer Measurements and Predictions for a Modern, High-Pressure, Transonic Turbine, Including Endwalls 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 002:;page 21001
    Author(s): James A. Tallman; Charles W. Haldeman; Anil K. Tolpadi; Robert F. Bergholz; Michael G. Dunn
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents both measurements and predictions of the hot-gas-side heat transfer to a modern, 112 stage high-pressure, transonic turbine. Comparisons of the predicted and measured heat ...
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