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    Unsteady Work Transfer Within a Turbine Blade Row Passage 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 009:;page 91001
    Author(s): Rose, Martin G.; Marx, Martin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: There is evidence in the literature of strong static pressure pulsation on the suction and pressure sides of turbine aerofoil rows experiencing unsteady wake interaction from upstream blade rows. This evidence is both ...
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    The Thermodynamics of Wake Blade Interaction in Axial Flow Turbines: Combined Experimental and Computational Study 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 003:;page 31015
    Author(s): Rose, Martin; Schأ¼pbach, Peter; Mansour, Michel
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports on insights into the detailed thermodynamics of axial turbine nozzle guide vane (NGV) wakes as they interact with the rotor blades. The evidence presented is both computational and experimental. Unsteady ...
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    Experimentally Observed Unsteady Work at Inlet to and Exit From an Axial Flow Turbine Rotor 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 006:;page 61017
    Author(s): Rose, Martin G.; Jenny, Philipp; Gier, Jochen; Abhari, Reza S.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: World literature has introduced the aerodynamic importance of unsteadiness in turbines. In particular, the unsteady static pressure field determines the work of the machine. The unsteadiness can redistribute the total ...
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    Blade–Row Interactions in a Low Pressure Turbine at Design and Strong Off Design Operation 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 011:;page 111002
    Author(s): Lipfert, Martin; Habermann, Jan; Rose, Martin G.; Staudacher, Stephan; Guendogdu, Yavuz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a joint project between the Institute of Aircraft Propulsion Systems (ILA) and MTU Aero Engines, a twostage low pressure turbine is tested at design and strong offdesign conditions. The experimental data taken in the ...
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    A Low Pressure Turbine at Extreme Off Design Operation 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 003:;page 31018
    Author(s): Lipfert, Martin; Marx, Martin; Rose, Martin G.; Staudacher, Stephan; Mahle, Inga; Freygang, Udo; Brettschneider, Markus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a cooperative project between the Institute of Aircraft Propulsion Systems and MTU Aero Engines GmbH, a twostage low pressure turbine with integrated 3D airfoil and endwall contouring is tested. The experimental data ...
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    Development and Application of a Fast-Response Total Temperature Probe for Turbomachinery 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 005:;page 51010
    Author(s): Arenz, Martin C.; Weigel, Björn; Habermann, Jan; Staudacher, Stephan; Rose, Martin G.; Berns, Wolfgang; Lutum, Ewald
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The measurement of unsteady total temperature is of great interest for the examination of loss mechanisms in turbomachinery with respect to the improvement of the efficiency. Since conventional thermocouples are limited ...
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