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    Experimental Investigation of Pressure Side Flow Separation on the T106C Airfoil at High Suction Side Incidence Flow 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 005:;page 51007
    Author(s): Stotz, Stephan; Guendogdu, Yavuz; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of this work is to study the influence of a pressure side separation bubble on the profile losses and the development of the bubble in the blade passage. For the experimental investigations, the T106 profile ...
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    Hot Film Measurements on a Low Pressure Turbine Linear Cascade With Bypass Transition 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 009:;page 91007
    Author(s): Gomes, Reinaldo A.; Stotz, Stephan; Blaim, Franz; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Transition of the state of the boundary layer from laminar to turbulent plays an important role in the aerodynamic loss generation on turbine airfoils. An accurate simulation of the transition process and of the state of ...
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    On High-Resolution Pressure Amplitude and Phase Measurements Comparing Fast-Response Pressure Transducers and Unsteady Pressure-Sensitive Paint 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 003:;page 031012-1
    Author(s): Bitter, Martin; Stotz, Stephan; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the simultaneous application of fast-response pressure transducers and unsteady pressure-sensitive paint (unsteady PSP) for the precise determination of pressure amplitudes and phases up to 3000 Hz. ...
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