Add to ORKGIn this study, a design procedure incorporating a genetic algorithm (GA) is developed for optimization of the wing structure of a two seated trainer aircraft with single turboprop engine. The objective function considered is the total weight of the structure. The objective function is minimized subjected to certain strength requirements. In order to evaluate the design constraints and model the wing structure, finite element analysis is performed by using a conventional finite element solver (i.e. MSC/NASTRAN®). In addition, MSC/PATRAN® commercial package program is used as preprocessor and postprocessor tool. VISUAL FORTRAN programming language is also utilized as the genetic algorithm implementation tool. Several conclusions drawn from th...
Presented diploma thesis deals with parametric optimization of wing caisson of L 410 NG aircraft to ...
This paper presents a wing aerostructural optimization framework based on the Individual Discipline ...
In order to pre-size a fuselage section, an optimisation process based on genetic algorithms is deve...
As a multi-disciplinary optimization problem, aerostructural shape optimization of airplane wings re...
The design of aircraft wings can be examined in two ways, namely, by aerodynamic analysis and by str...
Bu çalışmada, optimizasyon çalışmalarında diğer tekniklere nazaran daha yeni bir yöntem olan Genetik...
This work focuses on the implementation of a complex multidisciplinary computational environment for...
A quasi-three-dimensional aerodynamic solver is integrated with a semi-analytical structural weight ...
302-307Aircraft design is a highly nonlinear problem and inherently multidisciplinary activity that...
Aircraft wings have seen very few changes in the topological arrangement of the internal structures ...
In this study an automated multidisciplinary design optimization code is developed for the minimum w...
The design of the wings for a transonic civil transport aircraft is an extremely complex task. It is...
Optimal design of complex engineering systems, such as aircraft composite structures, can often be a...
The quest for finding optimum solutions to engineering problems has existed for a long time. In the ...
Structural optimization is achieving the best objective function from a predefined medium, well boun...
Presented diploma thesis deals with parametric optimization of wing caisson of L 410 NG aircraft to ...
This paper presents a wing aerostructural optimization framework based on the Individual Discipline ...
In order to pre-size a fuselage section, an optimisation process based on genetic algorithms is deve...
As a multi-disciplinary optimization problem, aerostructural shape optimization of airplane wings re...
The design of aircraft wings can be examined in two ways, namely, by aerodynamic analysis and by str...
Bu çalışmada, optimizasyon çalışmalarında diğer tekniklere nazaran daha yeni bir yöntem olan Genetik...
This work focuses on the implementation of a complex multidisciplinary computational environment for...
A quasi-three-dimensional aerodynamic solver is integrated with a semi-analytical structural weight ...
302-307Aircraft design is a highly nonlinear problem and inherently multidisciplinary activity that...
Aircraft wings have seen very few changes in the topological arrangement of the internal structures ...
In this study an automated multidisciplinary design optimization code is developed for the minimum w...
The design of the wings for a transonic civil transport aircraft is an extremely complex task. It is...
Optimal design of complex engineering systems, such as aircraft composite structures, can often be a...
The quest for finding optimum solutions to engineering problems has existed for a long time. In the ...
Structural optimization is achieving the best objective function from a predefined medium, well boun...
Presented diploma thesis deals with parametric optimization of wing caisson of L 410 NG aircraft to ...
This paper presents a wing aerostructural optimization framework based on the Individual Discipline ...
In order to pre-size a fuselage section, an optimisation process based on genetic algorithms is deve...