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    Influence of Loading Distribution on the Off-Design Performance of High-Pressure Turbine Blades 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003:;page 563
    Author(s): D. Corriveau; S. A. Sjolander
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Linear cascade measurements for the aerodynamic performance of a family of three transonic, high-pressure (HP) turbine blades have been presented previously by the authors. The airfoils were ...
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    Effect of Geometry on the Performance of Radial Vaneless Diffusers 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 004:;page 550
    Author(s): Yingkang Zhu; S. A. Sjolander
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents measurements of the steady aerodynamic characteristics of a series of five radial vaneless diffusers with walls varying from mildly divergent to strongly convergent. The static ...
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    Development of the Tip-Leakage Flow Downstream of a Planar Cascade of Turbine Blades: Vorticity Field 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004:;page 609
    Author(s): M. Yaras; S. A. Sjolander
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents detailed measurements of the tip-leakage flow emerging from a planar cascade of turbine blades. Four clearances of from 1.5 to 5.5 percent of the blade chord are considered. ...
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    Measurements of the Flow in an Idealized Turbine Tip Gap 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004:;page 578
    Author(s): S. A. Sjolander; D. Cao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: To gain further insights into the details of the tip-gap flow in axial turbines, a test section has been constructed with a single idealized, large-scale tip gap. The single “blade” forms a ...
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    Effects of Tip Clearance on Blade Loading in a Planar Cascade of Turbine Blades 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 002:;page 237
    Author(s): S. A. Sjolander; K. K. Amrud
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper examines in detail the structure of the tip leakage flow and its effect on the blade loading in a large-scale planar cascade of turbine blades. The tip clearance was varied from ...
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    Flow Field in the Tip Gap of a Planar Cascade of Turbine Blades 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 003:;page 276
    Author(s): M. Yaras; Yingkang Zhu; S. A. Sjolander
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements are presented for the flow in the tip gap of a planar cascade of turbine blades. Three clearances of from 2.0 to 3.2 percent of the blade chord were considered. Detailed surveys ...
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    Effects of Simulated Rotation on Tip Leakage in a Planar Cascade of Turbine Blades: Part I—Tip Gap Flow 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 003:;page 652
    Author(s): M. I. Yaras; S. A. Sjolander
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents further results from a continuing study on tip leakage in axial turbines. Rotation has been simulated in a linear cascade test section by using a moving-belt tip wall. ...
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    Prediction of Tip-Leakage Losses in Axial Turbines 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 204
    Author(s): M. I. Yaras; S. A. Sjolander
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Existing methods for predicting the tip-leakage losses in turbomachinery are based on a variety of assumptions, many of which have not been fully verified experimentally. Recently, several detailed ...
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    An Empirical Prediction Method for Secondary Losses in Turbines—Part I: A New Loss Breakdown Scheme and Penetration Depth Correlation 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 002:;page 273
    Author(s): M. W. Benner; S. A. Sjolander; S. H. Moustapha
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Despite its wide use in meanline analyses, the conventional loss breakdown scheme is based on a number of assumptions that are known to be physically unsatisfactory. One of these assumptions ...
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    An Empirical Prediction Method For Secondary Losses In Turbines—Part II: A New Secondary Loss Correlation 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 002:;page 281
    Author(s): M. W. Benner; S. A. Sjolander; S. H. Moustapha
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new empirical prediction method for design and off-design secondary losses in turbines has been developed. The empirical prediction method is based on a new loss breakdown scheme, and as ...
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