Add to ORKGA parallel design platform is developed for aerostructural shape optimization of airplane wings. The developed tools consist of a panel method-based aerodynamic solver, a finite element-based structural solver, geometry and mesh generation modules and a parallel genetic algorithm optimizer, with emphasis given to automation and fast solution
This paper presents a wing aerostructural optimization framework based on the Indi-vidual Discipline...
A strategy is presented to optimize wing structures under static aeroelastic constraints with respec...
A method is presented for concurrent aerostructural optimization of wing planform, airfoil and high ...
As a multi-disciplinary optimization problem, aerostructural shape optimization of airplane wings re...
AbstractThe paper addresses an application of the software product OPTIMENGA_AERO to a real-life des...
A new bilevel optimization strategy for wing design is developed, in which the optimizations of the ...
As computing technology improves, and the need for better designed aircraft structures rises, enhanc...
This paper describes a parallel multi-criteria (multi-objective) evolutionary algorithm for aero-str...
A series of novel algorithms for performing aerostructural shape and topology optimization are intro...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83550/1/AIAA-2010-9308-579.pd
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...
The demand for more efficient and lighter structural components has shifted focus to formal optimiza...
This thesis is motivated by the desire to discover fuel efficient aircraft concepts through explorat...
This thesis presents new tools and techniques developed to address the challenging problem of high-f...
This paper presents a wing aerostructural optimization framework based on the Indi-vidual Discipline...
A strategy is presented to optimize wing structures under static aeroelastic constraints with respec...
A method is presented for concurrent aerostructural optimization of wing planform, airfoil and high ...
As a multi-disciplinary optimization problem, aerostructural shape optimization of airplane wings re...
AbstractThe paper addresses an application of the software product OPTIMENGA_AERO to a real-life des...
A new bilevel optimization strategy for wing design is developed, in which the optimizations of the ...
As computing technology improves, and the need for better designed aircraft structures rises, enhanc...
This paper describes a parallel multi-criteria (multi-objective) evolutionary algorithm for aero-str...
A series of novel algorithms for performing aerostructural shape and topology optimization are intro...
Advances in numerical optimization have raised the possibility that efficient and novel aircraft con...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83550/1/AIAA-2010-9308-579.pd
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...
The demand for more efficient and lighter structural components has shifted focus to formal optimiza...
This thesis is motivated by the desire to discover fuel efficient aircraft concepts through explorat...
This thesis presents new tools and techniques developed to address the challenging problem of high-f...
This paper presents a wing aerostructural optimization framework based on the Indi-vidual Discipline...
A strategy is presented to optimize wing structures under static aeroelastic constraints with respec...
A method is presented for concurrent aerostructural optimization of wing planform, airfoil and high ...