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    Time-Marching Analysis of Steady Transonic Flow in Turbomachinery Cascades Using the Hopscotch Method 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002:;page 272
    Author(s): R. A. Delaney
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A rapid, time-marching, numerical scheme based on the hopscotch method is presented for solution of steady, two-dimensional, transonic flow in turbomachinery cascades. The scheme is applied to ...
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    Transonic Flow Analysis in Axial-Flow Turbomachinery Cascades by a Time-Dependent Method of Characteristics 

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 003:;page 356
    Author(s): R. A. Delaney; P. Kavanagh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Solutions for transonic flow in cascades are determined by a second-order time-dependent method of characteristics using bicharacteristics. The analysis method is based on unsteady, two-dimensional, ...
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    Study of Three-Dimensional Viscous Flows in an Axial Compressor Cascade Including Tip Leakage Effects Using a SIMPLE-Based Algorithm 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001:;page 51
    Author(s): M. Pouagare; R. A. Delaney
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A multisweep space-marching solver based on a modified version of the SIMPLE algorithm was employed to study the three-dimensional flow field through a linear cascade. Three cases were tested: ...
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    An Accurate and Efficient Euler Solver for Three-Dimensional Turbomachinery Flows 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003:;page 346
    Author(s): C. F. Shieh; R. A. Delaney
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Accurate and efficient Euler equation numerical solution techniques are presented for analysis of three-dimensional turbomachinery flows. These techniques include an efficient explicit hopscotch ...
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    Solution Procedure for Unsteady Two-Dimensional Boundary Layers 

    Source: Journal of Fluids Engineering:;1988:;volume( 110 ):;issue: 001:;page 69
    Author(s): O. Key Kwon; R. H. Pletcher; R. A. Delaney
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An accurate and reliable solution procedure is presented for solving the two-dimensional, compressible, unsteady boundary layer equations. The procedure solves the governing equations in a coupled ...
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    Analysis of Three-Dimensional Turbomachinery Flows on C-Type Grids Using an Implicit Euler Solver 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 362
    Author(s): K. F. Weber; D. W. Thoe; R. A. Delaney
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A three-dimensional Euler analysis for turbomachinery flows on a C-type grid is presented. The analysis is based on the Beam and Warming implicit algorithm for solution of the unsteady Euler ...
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    Calculation of Unsteady Turbulent Boundary Layers 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 002:;page 195
    Author(s): O. K. Kwon; R. H. Pletcher; R. A. Delaney
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An unsteady, two-dimensional boundary-layer solution procedure is used to predict two different types of incompressible turbulent mean flows, the Blasius and Howarth flows, with superimposed ...
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    Numerical Prediction of Turbine Vane-Blade Aerodynamic Interaction 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 004:;page 387
    Author(s): J. P. Lewis; R. A. Delaney; E. J. Hall
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A time-accurate analysis for turbine vane-blade interaction is presented. The analysis simultaneously solves the unsteady isentropic Euler equations in the vane and blade rows on a blade-to-blade ...
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    Investigation of Unsteady Flow Through a Transonic Turbine Stage: Data/Prediction Comparison for Time-Averaged and Phase-Resolved Pressure Data 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 91
    Author(s): M. G. Dunn; W. A. Bennett; R. A. Delaney; K. V. Rao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents time-averaged and phase-resolved measurements of the surface pressure data for the vane and blade of a transonic single-stage research turbine. The data are compared and ...
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    Influence of Vane-Blade Spacing on Transonic Turbine Stage Aerodynamics: Part I—Time-Averaged Data and Analysis 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 004:;page 663
    Author(s): B. L. Venable; J. A. Busby; M. G. Dunn; C. W. Haldeman; R. L. Davis; R. A. Delaney; D. J. Dorney; R. S. Abhari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A comprehensive study has been performed to determine the influence of vane-blade spacing on transonic turbine stage aerodynamics. In Part I of this paper, an investigation of the effect of ...
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