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    Effects of Reynolds Number and Free-Stream Turbulence on Boundary Layer Transition in a Compressor Cascade 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 001:;page 1
    Author(s): Heinz-Adolf Schreiber; Bernhard Küsters; Wolfgang Steinert
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental and analytical study has been performed on the effect of Reynolds number and free-stream turbulence on boundary layer transition location on the suction surface of a controlled ...
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    1999 Turbomachinery Committee Best Paper Award: Development of Advanced Compressor Airfoils for Heavy-Duty Gas Turbines— Part I: Design and Optimization 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 003:;page 397
    Author(s): Ulf Köller; Bernhard Küsters; Heinz-Adolf Schreiber; Reinhard Mönig
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new family of subsonic compressor airfoils, which are characterized by low losses and wide operating ranges, has been designed for use in heavy-duty gas turbines. In particular the influence ...
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    1999 Turbomachinery Committee Best Paper Award: Development of Advanced Compressor Airfoils for Heavy-Duty Gas Turbines— Part II: Experimental and Theoretical Analysis 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 003:;page 406
    Author(s): Bernhard Küsters; Ulf Köller; Reinhard Mönig; Heinz-Adolf Schreiber
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In Part I of this paper a family of numerically optimized subsonic compressor airfoils for heavy-duty gas turbines, covering a wide range of flow properties, is presented. The objective of the ...
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