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    Blade Design of Axial-Flow Compressors by the Method of Optimal Control Theory—Application of Pontryagin’s Maximum Principles, a Sample Calculation and Its Results 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 001:;page 103
    Author(s): Chuan-gang Gu; Yong-miao Miao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Using the continual transformation technique [3] and the augmented penalty function method, the typical optimal control problem with various constraints proposed in the paper [2] has been converted ...
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    Blade Design of Axial-Flow Compressors by the Method of Optimal Control Theory—Physical Model and Mathematical Expression 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 001:;page 99
    Author(s): Chuan-gang Gu; Yong-miao Miao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the design of compressor blades we put forward an optimization flow-type problem which enables the designers to consider the optimization of specified performance index of the flow-type ...
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    Experimental Investigations of Flows Through a Plane Cascade at Large Angles of Attack With Separations 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 003:;page 323
    Author(s): Chuan-Gang Gu; Lai-Qin Luo; Yong-Miao Miao
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements of various parameters in the flows through a cascade at different angles of attack have been performed. The parameters, such as Reynolds stresses (uu /U2 , vv /U2 , and uv /U2 ...
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