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Interaction of Compressor Rotor Blade Wake With Wall Boundary Layer/Vortex in the End-Wall Region
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 ...
Erratum: “Rotor Wake Mixing Effects Downstream of a Compressor Rotor” (Journal of Engineering for Power, 1982, 104, pp. 202–210)
Publisher: The American Society of Mechanical Engineers (ASME)
Rotor Wake Mixing Effects Downstream of a Compressor Rotor
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 ...
Structure and Decay Characteristics of Turbulence in the Near and Far-Wake of a Moderately Loaded Compressor Rotor-Blade
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 ...
Mean Velocity and Decay Characteristics of the Near and Far-Wake of a Compressor Rotor Blade of Moderate Loading
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 ...
Conventional Probes for the Relative Flow Measurement in a Turbomachinery Rotor Blade Passage
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 ...
Mitigation of Fretting Fatigue Damage in Blade and Disk Pressure Faces With Low Plasticity Burnishing
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 ...
Improved High Cycle Fatigue Damage Tolerance of Turbine-Engine Compressor Components by Low Plasticity Burnishing
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. ...
Case Studies of Fatigue Life Improvement Using Low Plasticity Burnishing in Gas Turbine Engine Applications
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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