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    Optimization of Multiple Jets Mixing With a Confined Crossflow 

    Source: Journal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 002:;page 315
    Author(s): Th. Doerr; M. Blomeyer; D. K. Hennecke
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation of a nonreacting multiple jet mixing with a confined crossflow has been conducted. Flow and geometric conditions were varied in order to examine favorable parameters ...
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    Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings: Part I—A Model for Subsonic Flow 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 001:;page 73
    Author(s): W. M. König; L. Fottner; D. K. Hennecke
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: New blading concepts as used in modern transonic axial-flow compressors require improved loss and deviation angle correlations. The new model presented in this paper incorporates several elements ...
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    Improved Blade Profile Loss and Deviation Angle Models for Advanced Transonic Compressor Bladings: Part II—A Model for Supersonic Flow 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 001:;page 81
    Author(s): W. M. König; L. Fottner; D. K. Hennecke
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: New blading concepts as used in modern transonic axial-flow compressors require improved loss and deviation angle correlations. The new model presented in this paper incorporates several elements ...
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