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    Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines—Part I: Methodology and Verification 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21011
    Author(s): D. X. Wang; L. He
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The adjoint method for blade design optimization will be described in this two-part paper. The main objective is to develop the capability of carrying out aerodynamic blading shape design ...
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    Concurrent Blade Aerodynamic-Aero-elastic Design Optimization Using Adjoint Method 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001:;page 11021
    Author(s): L. He; D. X. Wang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Increasing aerothermal and aero-elastic performance requirements and constraints are closely linked in modern blading designs. There is thus a need for more concurrent interaction between the ...
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    Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines—Part II: Validation and Application 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 002:;page 21012
    Author(s): D. X. Wang; L. He; Y. S. Li; R. G. Wells
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This is the second part of a two-part paper. First, the design-optimization system based on the adjoint gradient solution approach as described in Part I is introduced. Several test cases are ...
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