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    Turbulence Intensity and Length Scale Measurements in Multistage Compressors 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001:;page 38
    Author(s): T. R. Camp; H.-W. Shin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the measurement and processing of turbulence data from multistage low-speed compressors. Measurements were made at the same relative positions in three four-stage compressors, ...
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    Design and Test of an Ultralow Solidity Flow-Controlled Compressor Stator 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 004:;page 689
    Author(s): K. R. Kirtley; P. Wood; B. Beacher; P. Graziosi; H.-W. Shin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A full annulus fluidic flow-controlled compressor stator ring was designed and tested in the third stage of a four-stage low-speed research compressor. The solidity of the flow-controlled stator ...
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    Boundary Layer Development in Axial Compressors and Turbines: Part 1 of 4—Composite Picture 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001:;page 114
    Author(s): T. H. Okiishi; G. J. Walker; H. P. Hodson; H.-W. Shin; D. E. Halstead; D. C. Wisler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Comprehensive experiments and computational analyses were conducted to understand boundary layer development on airfoil surfaces in multistage, axial-flow compressors and LP turbines. The tests were ...
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    Boundary Layer Development in Axial Compressors and Turbines: Part 3 of 4— LP Turbines 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 002:;page 225
    Author(s): T. H. Okiishi; G. J. Walker; H. P. Hodson; H.-W. Shin; D. E. Halstead; D. C. Wisler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This is Part Three of a four-part paper. It begins with Section 11.0 and continues to describe the comprehensive experiments and computational analyses that have led to a detailed picture of ...
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    Boundary Layer Development in Axial Compressors and Turbines: Part 2 of 4—Compressors 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003:;page 426
    Author(s): T. H. Okiishi; G. J. Walker; H. P. Hodson; H.-W. Shin; D. E. Halstead; D. C. Wisler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This is Part Two of a four-part paper. It begins with Section 6.0 and continues to describe the comprehensive experiments and computational analyses that have led to a detailed picture of ...
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    Boundary Layer Development in Axial Compressors and Turbines: Part 4 of 4—Computations and Analyses 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001:;page 128
    Author(s): T. H. Okiishi; G. J. Walker; H. P. Hodson; H.-W. Shin; D. E. Halstead; D. C. Wisler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This is Part Four of a four-part paper. It begins with Section 16.0 and concludes the description of the comprehensive experiments and computational analyses that have led to a detailed picture ...
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    Effects of Rotating Inlet Distortion on Multistage Compressor Stability 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 181
    Author(s): J. P. Longley; H. -W. Shin; R. E. Plumley; I. J. Day; E. M. Greitzer; D. C. Wisler; C. S. Tan; P. D. Silkowski
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In multispool engines, rotating stall in an upstream compressor will impose a rotating distortion on the downstream compressor, thereby affecting its stability margin. In this paper experiments ...
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    Effects of Nonaxisymmetric Tip Clearance on Axial Compressor Performance and Stability 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 648
    Author(s): M. B. Graf; H.-W. Shin; D. C. Wisler; T. S. Wong; E. M. Greitzer; F. E. Marble; C. S. Tan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of circumferentially nonuniform tip clearance on axial compressor performance and stability have been investigated experimentally and analytically. A theoretical model for compressor ...
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    Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors: Part I—Experiment 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 003:;page 433
    Author(s): A. F. Storace; F. F. Ehrich; S. J. Song; Z. S. Spakovszky; D. C. Wisler; H.-W. Shin; M. Martinez-Sanchez; B. F. Beacher
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental and theoretical investigation has been conducted to evaluate the effects seen in axial-flow compressors when the centerline of the rotor is displaced from the centerline of the ...
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    Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors: Part II—Analysis 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 003:;page 446
    Author(s): S. J. Song; D. C. Wisler; F. F. Ehrich; Z. S. Spakovszky; A. F. Storace; H.-W. Shin; M. Martinez-Sanchez; B. F. Beacher
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental and theoretical investigation was conducted to evaluate the effects seen in axial-flow compressors when the centerline of the rotor becomes displaced from the centerline of the ...
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