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    Design of Turbomachinery Blading in Transonic Flows by the Circulation Method 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 141
    Author(s): T. Q. Dang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The newly developed three-dimensional design technique for turbomachinery blading based on the circulation method has been successfully extended into the transonic flow regime. The main task ...
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    A Fully Three-Dimensional Inverse Method for Turbomachinery Blading in Transonic Flows 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002:;page 354
    Author(s): T. Q. Dang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a procedure to extend a recently developed fully three-dimensional inverse method for highly loaded turbomachine blades into the transonic-flow regime. In this inverse method, ...
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    Throughflow Method for Turbomachines Applicable for All Flow Regimes 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 002:;page 256
    Author(s): S. V. Damle; D. R. Reddy; T. Q. Dang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new axisymmetric throughflow method for analyzing and designing turbomachines is proposed. This method utilizes body-force terms to represent blade forces and viscous losses. The resulting ...
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    Improving Aerodynamic Matching of Axial Compressor Blading Using a Three-Dimensional Multistage Inverse Design Method 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 001:;page 108
    Author(s): M. P. C. van Rooij; L. M. Larosiliere; T. Q. Dang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Current turbomachinery design systems increasingly rely on multistage CFD as a means to diagnose designs and assess performance potential. However, design weaknesses attributed to improper stage ...
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