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    The Feasibility of Water Injection Into the Turbine Coolant to Permit Gas Turbine Contingency Power for Helicopter Application 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 003:;page 635
    Author(s): G. J. Van Fossen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A system which would allow a substantially increased output from a turboshaft engine for brief periods in emergency situations with little or no loss of turbine stress rupture life is proposed ...
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    Heat-Transfer Coefficients for Staggered Arrays of Short Pin Fins 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002:;page 268
    Author(s): G. J. VanFossen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Short pin fins are often used to increase the heat transfer to the coolant in the trailing edge of a turbine blade. Due primarily to limits of casting technology, it is not possible to ...
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    Length to Diameter Ratio and Row Number Effects in Short Pin Fin Heat Transfer 

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 001:;page 241
    Author(s): B. A. Brigham; G. J. VanFossen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recently, several experiments concerning heat transfer from short pin fins have been conducted with the results indicating lower heat transfer from short pin fins than from longer pin fins found ...
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    Endwall Heat Transfer Measurements in a Transonic Turbine Cascade 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002:;page 305
    Author(s): P. W. Giel; D. R. Thurman; G. J. Van Fossen; S. A. Hippensteele; R. J. Boyle
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbine blade endwall heat transfer measurements are presented for a range of Reynolds and Mach numbers. Data were obtained for Reynolds numbers based on inlet conditions of 0.5 and 1.0 × ...
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    Three-Dimensional Navier–Stokes Analysis and Redesign of an Imbedded Bellmouth Nozzle in a Turbine Cascade Inlet Section 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 003:;page 529
    Author(s): P. W. Giel; I. Lopez; G. J. Van Fossen; J. R. Sirbaugh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental measurements in the inlet of a transonic turbine blade cascade showed unacceptable pitchwise flow nonuniformity. A three-dimensional, Navier–Stokes computational fluid dynamics (CFD) ...
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