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    Compressor Erosion and Performance Deterioration 

    Source: Journal of Fluids Engineering:;1987:;volume( 109 ):;issue: 003:;page 297
    Author(s): W. Tabakoff
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Aircraft engines operating in areas where the atmosphere is polluted by small solid particles are typical examples of jet engines operating under hostile atmospheric environment. The particles ...
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    Review—Turbomachinery Performance Deterioration Exposed to Solid Particulates Environment 

    Source: Journal of Fluids Engineering:;1984:;volume( 106 ):;issue: 002:;page 125
    Author(s): W. Tabakoff
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of this paper is to review experimental and analytical investigations concerning the effect of the presence of solid particles on the performance of turbomachines. Experimental data ...
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    Discussion: “Calculation of Compressible Subsonic Flow in Cascades With Varying Blade Height” (Van den Braembussche, R. A., 1973, ASME J. Eng. Power, 95, pp. 345–351) 

    Source: Journal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 003:;page 319
    Author(s): W. Tabakoff
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Some Effects of Variable Surface Temperature on Heat Transfer to a Partially Porous Flat Plate” (Nealy, D. A., 1973, ASME J. Eng. Power, 95, pp. 319–325) 

    Source: Journal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 003:;page 320
    Author(s): W. Tabakoff
    Publisher: The American Society of Mechanical Engineers (ASME)
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    A Study of the Surface Deterioration due to Erosion 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 004:;page 834
    Author(s): W. Tabakoff; C. Balan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbomachines are subject to an excessive rate of erosion when operated in dusty environments or exposed to combustion gases of newly developed synthetic fuels or heavy oils. The surface quality ...
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    Coating Effect on Particle Trajectories and Turbine Blade Erosion 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002:;page 250
    Author(s): W. Tabakoff; M. Metwally
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbine engines operating in dusty environments are exposed to erosion and performance deterioration. In order to improve the erosion resistance, nickel and cobalt superalloy blades and vanes ...
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    The Dynamics of Suspended Solid Particles in a Two-Stage Gas Turbine 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 002:;page 298
    Author(s): W. Tabakoff; A. Hamed
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbine engines operating in dusty environments are exposed to erosion and performance deterioration. In order to provide the basis for calculating the erosion and performance deterioration ...
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    Erosion Study of Radial Flow Compressor With Splitters 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 001:;page 62
    Author(s): S. Elfeki; W. Tabakoff
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas turbine engines operating in areas where the atmosphere is polluted by small solid particles are examples of machines operating under particulate two-phase flow conditions. The presence of ...
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    Temperature Effect on Particle Dynamics and Erosion in Radial Inflow Turbine 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 002:;page 258
    Author(s): W. Tabakoff; A. Hamed
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the results of an investigation of the particle dynamics and the resulting blade erosion in radial inflow turbine rotors. In order to determine the influence of the ...
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    Effect of Inlet Flow Angle on the Erosion of Radial Turbine Guide Vanes 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001:;page 64
    Author(s): H. Eroglu; W. Tabakoff
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The results of an investigation of the particle dynamics and the blade erosion at the impact locations in radial turbine guide vanes are presented. Attention is focused in particular on the ...
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