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    Contributions to the Measurement and Calculation of Stresses in Plane Rotating Disks Without Rotational Symmetry 

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003:;page 315
    Author(s): H. E. Gallus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper gives details of the experimental and theoretical work of the author on the above-mentioned subject. The first part of the paper deals with the experimental investigations of plane ...
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    An Analysis Method for Multistage Transonic Turbines With Coolant Mass Flow Addition 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 744
    Author(s): F. Mildner; H. E. Gallus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The subject of this paper is a numerical method for the calculation of the transonic flow field of multistage turbines, taking high coolant flow into account. To reduce the processing time, ...
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    Monitoring of Aerodynamic Load and Detection of Stall in Multistage Axial Compressors 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001:;page 81
    Author(s): H. Hönen; H. E. Gallus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady flow in a single-stage axial flow compressor at different operating conditions has been investigated with hot-wire and hot-film probes to find out the influence of the aerodynamic ...
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    Effects of Stator Wakes and Spanwise Nonuniform Inlet Conditions on the Rotor Flow of an Axial Turbine Stage 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001:;page 128
    Author(s): J. Zeschky; H. E. Gallus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed measurements have been performed in a subsonic, axial-flow turbine stage to investigate the structure of the secondary flow field and the loss generation. The data include the static ...
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    Three-Dimensional Wake Decay Inside of a Compressor Cascade and Its Influence on the Downstream Unsteady Flow Field: Part II—Unsteady Flow Field Downstream of the Stator 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 190
    Author(s): C. Poensgen; H. E. Gallus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A measuring technique based on multisensor hot-wire anemometry has been developed to determine the unsteady three-dimensional velocity vector and the structure of turbulent flows. It then has ...
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    Three-Dimensional Wake Decay Inside of a Compressor Cascade and Its Influence on the Downstream Unsteady Flow Field: Part I—Wake Decay Characteristics in the Flow Passage 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 180
    Author(s): C. Poensgen; H. E. Gallus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A measuring technique based on multisensor hot-wire anemometry has been developed to determine the unsteady three-dimensional velocity vector and the structure of turbulent flows. It has then ...
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    The Influence of Blade Number Ratio and Blade Row Spacing on Axial-Flow Compressor Stator Blade Dynamic Load and Stage Sound Pressure Level 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003:;page 633
    Author(s): H. E. Gallus; H. Grollius; J. Lambertz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In axial-flow turbomachines considerable dynamic blade loads and noise production occur as a result of the unsteady blade row interaction between rotor and stator blades. This paper presents ...
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    Design and Rotor Performance of a 5:1 Mixed-Flow Supersonic Compressor 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 565
    Author(s): R. Mönig; W. Elmendorf; H. E. Gallus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In consideration of further jet-engine developments required by applications for supersonic travel aircraft, airbreathing propulsion of space vehicles, or only the improvement of conventional ...
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    Endwall and Unsteady Flow Phenomena in an Axial Turbine Stage 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004:;page 562
    Author(s): H. E. Gallus; C. Hah; J. Zeschky
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed experimental and numerical studies have been performed in a subsonic, axial-flow turbine stage to investigate the secondary flow field, the aerodynamic loss generation, and the spanwise ...
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    Rotating Stall in a Single-Stage Axial Flow Compressor 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 189
    Author(s): C. A. Poensgen; H. E. Gallus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the results on an experimental investigation of rotating stall flow inside a single-stage axial flow compressor. Tests were carried out in two steps. First, measurements ...
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