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    Interaction of Compressor Rotor Blade Wake With Wall Boundary Layer/Vortex in the End-Wall Region 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002:;page 467
    Author(s): B. Lakshminarayana; A. Ravindranath
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports the experimental study of the three-dimensional characteristics of the mean velocity of the rotor wake inside the annulus- and hub-wall boundary layers. The measurements were ...
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    Erratum: “Rotor Wake Mixing Effects Downstream of a Compressor Rotor” (Journal of Engineering for Power, 1982, 104, pp. 202–210) 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003:;page 722
    Author(s): A. Ravindranath; B. Takshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Rotor Wake Mixing Effects Downstream of a Compressor Rotor 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 001:;page 202
    Author(s): A. Ravindranath; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study of rotor wake was conducted in the trailing-edge and near-wake regions of a moderately loaded compressor rotor blade using a rotating triaxial hot-wire probe in a rotating ...
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    Structure and Decay Characteristics of Turbulence in the Near and Far-Wake of a Moderately Loaded Compressor Rotor-Blade 

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 001:;page 131
    Author(s): A. Ravindranath; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The wake of a turbomachinery rotor-blade is turbulent, highly three-dimensional, and nonisotropic with appreciable curvature in the trailing-edge and near-wake regions. The characteristics of the ...
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    Mean Velocity and Decay Characteristics of the Near and Far-Wake of a Compressor Rotor Blade of Moderate Loading 

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 003:;page 535
    Author(s): A. Ravindranath; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports the experimental study of the three-dimensional characteristics of the mean velocity in the wake of a moderately loaded compressor rotor blade. The measurements were taken ...
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    Conventional Probes for the Relative Flow Measurement in a Turbomachinery Rotor Blade Passage 

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002:;page 406
    Author(s): N. Sitaram; B. Lakshminarayana; A. Ravindranath
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports the measurement of the relative flow in the rotor blade passages of an axial-flow compressor and an axial-flow inducer using conventional probes such as five-hole, disk, and ...
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    Mitigation of Fretting Fatigue Damage in Blade and Disk Pressure Faces With Low Plasticity Burnishing 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 008:;page 82105
    Author(s): Paul S. Prevéy; Ravi A. Ravindranath; Michael Shepard; N. Jayaraman
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Low plasticity burnishing (LPB) is now established as a surface enhancement technology capable of introducing through-thickness compressive residual stresses in the edges of gas turbine engine ...
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    Improved High Cycle Fatigue Damage Tolerance of Turbine-Engine Compressor Components by Low Plasticity Burnishing 

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 001:;page 12102
    Author(s): Paul S. Prevéy; Ravi A. Ravindranath; Michael Shepard; N. Jayaraman
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Significant progress has been made in the application of low plasticity burnishing (LPB) technology to military engine components, leading to orders of magnitude improvement in damage tolerance. ...
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    Case Studies of Fatigue Life Improvement Using Low Plasticity Burnishing in Gas Turbine Engine Applications 

    Source: Journal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 004:;page 865
    Author(s): Paul S. Prevéy; Ravi A. Ravindranath; Michael Shepard; Timothy Gabb
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Surface enhancement technologies such as shot peening, laser shock peening, and low plasticity burnishing (LPB) can provide substantial fatigue life improvement. However, to be effective, the ...
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