The report reviews the TAU-Takanashi inverse design and the TAU adjoint gradient-based optimization process. The optimization process was successfully used for solving airfoil inverse design problems including optimizing lift, drag and pitching moment. For 3D inverse design Problems with twist, the TAU gradient-based optimization tried to approach to the target pressure distribution and geometry but a perfect match could not be achieved
This paper studies the effect of design variables vector on automatic aerodynamic shape optimization...
In the present work an extension of an aerodynamic optimization system for inverse design is carried...
Optimization of aerodynamic profiles is often done using methods based on coupling potential flow th...
With the increasing of computational power, the CFD has become a routine tool used for aerodynamic a...
Direct design optimisation methods for turbomachinery blades have consistently gained in popularity ...
The engineering problem of airfoil design has been of great theoretical interest for almost a centur...
Gradient-based optimization using the adjoint approach is a common method in shape optimization. Her...
A hybrid inverse/direct-optimization method for subsonic/transonic airfoil and wing shape design is ...
A classical inverse problem in fluid dynamics, i.e., determine the geometry of an airfoil given the ...
The increasing popularity of high fidelity computational fluid dynamics simulations in aerodynamic d...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
The aerodynamic inverse design approach consists of finding the ge-ometry that produces a desired (t...
This paper presents the fundamentals of a continuous adjoint method and the applications of this met...
Optimization algorithms are used in various engineering applications to identify optimal shapes. We ...
This paper studies the effect of design variables vector on automatic aerodynamic shape optimization...
In the present work an extension of an aerodynamic optimization system for inverse design is carried...
Optimization of aerodynamic profiles is often done using methods based on coupling potential flow th...
With the increasing of computational power, the CFD has become a routine tool used for aerodynamic a...
Direct design optimisation methods for turbomachinery blades have consistently gained in popularity ...
The engineering problem of airfoil design has been of great theoretical interest for almost a centur...
Gradient-based optimization using the adjoint approach is a common method in shape optimization. Her...
A hybrid inverse/direct-optimization method for subsonic/transonic airfoil and wing shape design is ...
A classical inverse problem in fluid dynamics, i.e., determine the geometry of an airfoil given the ...
The increasing popularity of high fidelity computational fluid dynamics simulations in aerodynamic d...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
Numerical shape optimization will play a strategic role for future aircraft design. It offers the po...
The aerodynamic inverse design approach consists of finding the ge-ometry that produces a desired (t...
This paper presents the fundamentals of a continuous adjoint method and the applications of this met...
Optimization algorithms are used in various engineering applications to identify optimal shapes. We ...
This paper studies the effect of design variables vector on automatic aerodynamic shape optimization...
In the present work an extension of an aerodynamic optimization system for inverse design is carried...
Optimization of aerodynamic profiles is often done using methods based on coupling potential flow th...