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    Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 2—External Aerodynamics, Total Pressure Losses, and Predictions 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 249
    Author(s): Oguz Uzol; Cengiz Camci
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Investigation of the internal fluid mechanic losses for a turbine blade with trailing edge coolant ejection was present in Uzol et al. (2001). The current study is a detailed experimental ...
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    Axial Flow Fan Tip Leakage Flow Control Using Tip Platform Extensions 

    Source: Journal of Fluids Engineering:;2010:;volume( 132 ):;issue: 005:;page 51109
    Author(s): Ali Aktürk; Cengiz Camci
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Performance of an axial flow fan unit is closely related to its tip leakage mass flow rate and level of tip/casing interactions. The present experimental study uses a stereoscopic particle ...
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    Aerodynamic Loss Characteristics of a Turbine Blade With Trailing Edge Coolant Ejection: Part 1—Effect of Cut-Back Length, Spanwise Rib Spacing, Free-Stream Reynolds Number, and Chordwise Rib Length on Discharge Coefficients 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 002:;page 238
    Author(s): Oguz Uzol; Boris Glezer; Cengiz Camci
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The internal fluid mechanics losses generated between the blade plenum chamber and a reference point located just downstream of the trailing edge are investigated for a turbine blade trailing ...
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    Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part II—Aerodynamic Measurements in the Rotational Frame 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 004:;page 697
    Author(s): Christopher McLean; Boris Glezer; Cengiz Camci; Professor of Aerospace Engineering
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current paper deals with the aerodynamic measurements in the rotational frame of reference of the Axial Flow Turbine Research Facility (AFTRF) at the Pennsylvania State University. Stationary ...
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    Mainstream Aerodynamic Effects Due to Wheelspace Coolant Injection in a High-Pressure Turbine Stage: Part I—Aerodynamic Measurements in the Stationary Frame 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 004:;page 687
    Author(s): Christopher McLean; Boris Glezer; Cengiz Camci; Professor of Aerospace Engineering
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The relative aerodynamic and performance effects associated with rotor–NGV gap coolant injections were investigated in the Axial Flow Turbine Research Facility (AFTRF) of the Pennsylvania State ...
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    Aerodynamics of Tip Leakage Flows Near Partial Squealer Rims in an Axial Flow Turbine Stage 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 001:;page 14
    Author(s): Cengiz Camci; Professor of Aerospace Engineering; Debashis Dey; Research Assistant; Levent Kavurmacioglu; Visiting Professor
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper deals with an experimental investigation of aerodynamic characteristics of full and partial-length squealer rims in a turbine stage. Full and partial-length squealer rims are investigated ...
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