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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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    Time Resolved Experimental Investigations of an Axial Compressor With Casing Treatment 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 001:;page 11018
    Author(s): R. Emmrich; H. Hönen; R. Niehuis
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A casing treatment with axial and radial skewed slots ending in a plenum chamber has experimentally been investigated at a highly subsonic axial compressor stage. The aim was to investigate ...
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    Experimental and Numerical Analysis of Gas Turbine Blades With Different Internal Cooling Geometries 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001:;page 11018
    Author(s): M. Eifel; V. Caspary; H. Hönen; P. Jeschke
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the effects of major geometrical modifications to the interior of a convection cooled gas turbine rotor blade. The analysis of the flow is performed experimentally with flow ...
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