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Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines—Part I: Methodology and Verification
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 ...
Concurrent Blade Aerodynamic-Aero-elastic Design Optimization Using Adjoint Method
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 ...
Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines—Part II: Validation and Application
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 ...