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    Hybrid RANS/LES Simulation of Corner Stall in a Linear Compressor Cascade 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 008:;page 81004
    Author(s): Xia, Guoping; Medic, Gorazd; Praisner, Thomas J.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Current design-cycle Reynolds-averaged Navier–Stokes (RANS) based computational fluid dynamics (CFD) methods have the tendency to over-predict corner-stall events for axial-flow compressors operating at off-design conditions. ...
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    Application of Endwall Contouring to Transonic Turbine Cascades: Experimental Measurements at Design Conditions 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 001:;page 11031
    Author(s): Taremi, Farzad; Sjolander, Steen A.; Praisner, Thomas J.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation of the endwall flows in two highturning turbine cascades was presented by Taremi et al. (2010, “Measurements of Endwall Flows in Transonic Linear Turbine Cascades: Part II—High Flow ...
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    Aerodynamics of a Low Pressure Turbine Airfoil at Low Reynolds Numbers—Part I: Steady Flow Measurements 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 001:;page 11010
    Author(s): Mahallati, Ali; McAuliffe, Brian R.; Sjolander, Steen A.; Praisner, Thomas J.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This twopart paper presents a detailed experimental investigation of the laminar separation and transition phenomena on the suction surface of a highlift lowpressure turbine airfoil, PakB. The first part describes the ...
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