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    A Review of Nonsteady Flow Models for Compressor Stability 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 002:;page 202
    Author(s): J. P. Longley
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a review of the different approaches to modeling the nonsteady fluid dynamics associated with two-dimensional compressor flow fields. These models are used to predict the ...
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    Stability of Flow Through Multistage Axial Compressors 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001:;page 126
    Author(s): J. P. Longley; T. P. Hynes
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes measurements of the performance of a research stage operating in isolation and as part of a multistage compressor. It is shown that the stall point and the stalled ...
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    Active Control of Rotating Stall in a Low-Speed Axial Compressor 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001:;page 48
    Author(s): J. D. Paduano; A. H. Epstein; L. Valavani; J. P. Longley; E. M. Greitzer; G. R. Guenette
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The onset of rotating stall has been delayed in a low-speed, single-stage, axial research compressor using active feedback control. Control was implemented using a circumferential array of hot ...
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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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