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    Discussion: “Experimental Study of the Flow Field Within a Transonic Axial Compressor Rotor by Laser Velocimetry and Comparison With Through-Flow Calculations” (Dunker, R. J., Strinning, P. E., and Weyer, H. B., 1978, ASME J. Eng. Power, 100, pp. 279–286) 

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 002:;page 286
    Author(s): Ch. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Turbulence and Unsteadiness Measurements Downstream of a Moving Blade Row” (Evans, R. L., 1975, ASME J. Eng. Power, 97, pp. 131–137) 

    Source: Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 001:;page 137
    Author(s): CH. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “A Nearly Three-Dimensional Intrablade Computing System for Turbomachinery” (Novak, R. A., and Hearsey, R. M., 1977, ASME J. Fluids Eng., 99, pp. 154–166) 

    Source: Journal of Fluids Engineering:;1977:;volume( 099 ):;issue: 001:;page 166
    Author(s): Ch. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    End-Wall Boundary Layers in Axial Compressors 

    Source: Journal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 004:;page 413
    Author(s): Ch. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Various aspects of an end-wall boundary-layer theory in axial compressors, as formulated originally by Mellor and Wood, are analyzed. This analysis contains three parts. In the first part the ...
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    Discussion: “An Experimental Study of Three-Dimensional Turbulent Boundary Layer and Turbulence Characteristics Inside a Turbomachinery Rotor Passage” (Anand, A. K., and Lakshminarayana, B., 1978, ASME J. Eng. Power, 100, pp. 676–687) 

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 004:;page 688
    Author(s): P. Kool; Ch. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Measurement of the Three-Dimensional Flow Field Behind an Axial Compressor Stage 

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 002:;page 168
    Author(s): Ch. Hirsch; P. Kool
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Hot wire instrumentation and a periodic sampling and averaging technique have been used in order to measure the three-dimensional flow field behind a rotor of an axial compressor stage. A ...
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    An Integrated Quasi-3D Finite Element Calculation Program for Turbomachinery Flows 

    Source: Journal of Engineering for Gas Turbines and Power:;1979:;volume( 101 ):;issue: 001:;page 141
    Author(s): Ch. Hirsch; G. Warzee
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A quasi-3D calculation program based on finite elements is presented in the spirit of Wu’s approach. In this work, however, the flow along the S2 surface is replaced by the calculation of ...
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    A Finite-Element Method for Through Flow Calculations in Turbomachines 

    Source: Journal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003:;page 403
    Author(s): Ch. Hirsch; G. Warzee
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new method for the numerical solution of the meridional through-flow equations in an axial flow machine is presented based on the finite-element method. A rigorous derivation of the pitch-averaged ...
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    Finite Element Methods for Transonic Blade-to-Blade Calculation in Turbomachines 

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 004:;page 665
    Author(s): H. Deconinck; Ch. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The transonic cascade flow is calculated with an efficient and flexible Galerkin Finite Element method applied to the full potential equation in Artificial Compressibility form. Some of the ...
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    Fluid–Structure Interaction Using a Modal Approach 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005:;page 51043
    Author(s): F. Debrabandere; B. Tartinville; G. Coussement; Ch. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new method for fluid‐structure interaction (FSI) predictions is here introduced, based on a reduced-order model (ROM) for the structure, described by its mode shapes and natural frequencies. ...
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