This thesis focuses on the development of a Computer-Aided-Design (CAD)-based geometry parameterization method and a corresponding surface mesh movement algorithm suitable for three-dimensional aerodynamic shape optimization. The geometry parameterization method includes a geometry control tool to aid in the construction and manipulation of a CAD geometry through a vendor-neutral application interface, CAPRI. It automates the tedious part of the construction phase involving data entry and providesintuitive and effective design variables that allow for both the flexibility and the precision required to control the movement of the geometry. The surface mesh movement algorithm, on the other hand, transforms an initial structured surface mesh t...
Reconciling optimized designs with the original model can be a time-consuming process. This thesis p...
The present paper focuses on the possibilities and strategies to model parametric and aircraft shape...
A Newton-Krylov algorithm is presented for aerodynamic shape optimization in three dimensions using ...
This thesis focuses on the development of a Computer-Aided-Design (CAD)-based geometry parameterizat...
The performance of an aerodynamic shape optimization routine is greatly dependent on its geometry co...
This thesis represents a step forward to bring geometry parameterization and control on par with the...
This thesis represents a step forward to bring geometry parameterization and control on par with the...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
The search for the most effective method for the geometric parameterization of many internal fluid f...
The objective for this paper is to present the development of an optimization capability for Curt3D,...
The geometry control method employed in an aerodynamic shape optimization algorithm defines what des...
The geometry control method employed in an aerodynamic shape optimization algorithm defines what des...
Design optimization methods using high-fidelity computational fluid dynamics simulations are becomin...
In the area of aircraft design, many studies about Multi Disciplinary Optimization (MDO) and Multi O...
Reconciling optimized designs with the original model can be a time-consuming process. This thesis p...
The present paper focuses on the possibilities and strategies to model parametric and aircraft shape...
A Newton-Krylov algorithm is presented for aerodynamic shape optimization in three dimensions using ...
This thesis focuses on the development of a Computer-Aided-Design (CAD)-based geometry parameterizat...
The performance of an aerodynamic shape optimization routine is greatly dependent on its geometry co...
This thesis represents a step forward to bring geometry parameterization and control on par with the...
This thesis represents a step forward to bring geometry parameterization and control on par with the...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
The search for the most effective method for the geometric parameterization of many internal fluid f...
The objective for this paper is to present the development of an optimization capability for Curt3D,...
The geometry control method employed in an aerodynamic shape optimization algorithm defines what des...
The geometry control method employed in an aerodynamic shape optimization algorithm defines what des...
Design optimization methods using high-fidelity computational fluid dynamics simulations are becomin...
In the area of aircraft design, many studies about Multi Disciplinary Optimization (MDO) and Multi O...
Reconciling optimized designs with the original model can be a time-consuming process. This thesis p...
The present paper focuses on the possibilities and strategies to model parametric and aircraft shape...
A Newton-Krylov algorithm is presented for aerodynamic shape optimization in three dimensions using ...