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    Unsteady Aerodynamic Blade Excitation at the Stability Limit and During Rotating Stall in an Axial Compressor 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003:;page 503
    Author(s): Ronald Mailach; Konrad Vogeler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The stable operating range of axial compressors is limited by the onset of rotating stall and surge. These flow conditions endanger the reliability of operation and definitely have to be avoided ...
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    Rotor-Stator Interactions in a Four-Stage Low-Speed Axial Compressor—Part I: Unsteady Profile Pressures and the Effect of Clocking 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 004:;page 507
    Author(s): Ronald Mailach; Konrad Vogeler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This two-part paper presents detailed experimental investigations of unsteady aerodynamic blade row interactions in the four-stage Low-Speed Research Compressor of Dresden. In part I of the paper ...
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    Aerodynamic Blade Row Interactions in an Axial Compressor—Part I: Unsteady Boundary Layer Development 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 001:;page 35
    Author(s): Ronald Mailach; Konrad Vogeler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This two-part paper presents experimental investigations of unsteady aerodynamic blade row interactions in the first stage of the four-stage low-speed research compressor of Dresden. Both the ...
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    Aerodynamic Blade Row Interactions in an Axial Compressor—Part II: Unsteady Profile Pressure Distribution and Blade Forces 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 001:;page 45
    Author(s): Ronald Mailach; Konrad Vogeler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This two-part paper presents experimental investigations of unsteady aerodynamic blade row interactions in the first stage of the four-stage low-speed research compressor of Dresden. Both the ...
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    Periodical Unsteady Flow Within a Rotor Blade Row of an Axial Compressor—Part II: Wake-Tip Clearance Vortex Interaction 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 004:;page 41005
    Author(s): Ronald Mailach; Ingolf Lehmann; Konrad Vogeler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this two-part paper, results of the periodical unsteady flow field within the third rotor blade row of the four-stage Dresden low-speed research compressor are presented. The main part of ...
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    Periodical Unsteady Flow Within a Rotor Blade Row of an Axial Compressor—Part I: Flow Field at Midspan 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 004:;page 41004
    Author(s): Ronald Mailach; Ingolf Lehmann; Konrad Vogeler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this two-part paper, results of the periodical unsteady flow field within the third rotor blade row of the four-stage Dresden low-speed research compressor are presented. The main part of ...
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    Rotor-Stator Interactions in a Four-Stage Low-Speed Axial Compressor—Part II: Unsteady Aerodynamic Forces of Rotor and Stator Blades 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 004:;page 519
    Author(s): Ronald Mailach; Lutz Müller; Konrad Vogeler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This two-part paper presents detailed experimental investigations of unsteady aerodynamic blade row interactions in the four-stage low-speed research compressor of Dresden. In Part I of the paper ...
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    Investigation of the Tip Clearance Flow in a Compressor Cascade Using a Novel Laser Measurement Technique With High Temporal Resolution 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005:;page 51004
    Author(s): Andreas Fischer; Marcel Gottschall; Ronald Mailach; Konrad Vogeler; Lars Büttner; Jürgen Czarske
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The understanding of the tip clearance flow in axial compressors is a key issue for developing new compressors with enhanced efficiency and reduced noise for instance. However, necessary flow ...
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