The PrandtlPlane (PrP) aircraft wing-box least-weight design is presented in this work. This design problem is formulated as a constrained non-linear programming problem (CNLPP), by integrating static, buckling, fatigue and manufacturability requirements, under different loading conditions. The solution search is carried out by means of a suitable multi-scale optimisation (MSO) approach. The physical responses involved into the CNLPP formulation are evaluated at the wing-box architecture level (macroscopic scale) and at the stiffened panel level (component scale), as well. The scale transition is ensured by means of a suitable global-local (GL) modelling approach, while the CNLPP is solved by means of an in-house genetic algorithm. The effe...
Abstract: Optimization of aerospace and lightweight structures, such as aircraft wings, is typ-icall...
This work focuses on the implementation of a complex multidisciplinary computational environment for...
The present Thesis deals with the application of optimization methods to the preliminary design of a...
The PrandtlPlane (PrP) aircraft wing-box least-weight design is presented in this work. This design ...
The PrandtlPlane (PrP) aircraft wing-box least-weight design is presented in this work. This design ...
In this work, a multi-scale optimization strategy for lightweight structures, based on a global-loca...
Air traffic passenger demand is constantly growing of about 5% per year. This will led to a substant...
In this work, a multi-scale optimization strategy for lightweight structures, based on a global-loca...
The paper aims at presenting and summarizing the activities carried out on the structural aspects of...
The paper describes a procedure, dedicated to the preliminary sizing of an aircraft wing-box, based ...
The present work takes origin from studies carried out at the Department of Aerospace Engineering of...
In this work, a design strategy for optimising thin-walled structures based on a global-local finite...
Aircrafts have become one of the most important modes of travel and have grown in the recent years. ...
The paper aims to present the phases and the achievements of the aerodynamic design activities carri...
The optimization of aerospace structures is a very complex problem, owing to the hundreds of design ...
Abstract: Optimization of aerospace and lightweight structures, such as aircraft wings, is typ-icall...
This work focuses on the implementation of a complex multidisciplinary computational environment for...
The present Thesis deals with the application of optimization methods to the preliminary design of a...
The PrandtlPlane (PrP) aircraft wing-box least-weight design is presented in this work. This design ...
The PrandtlPlane (PrP) aircraft wing-box least-weight design is presented in this work. This design ...
In this work, a multi-scale optimization strategy for lightweight structures, based on a global-loca...
Air traffic passenger demand is constantly growing of about 5% per year. This will led to a substant...
In this work, a multi-scale optimization strategy for lightweight structures, based on a global-loca...
The paper aims at presenting and summarizing the activities carried out on the structural aspects of...
The paper describes a procedure, dedicated to the preliminary sizing of an aircraft wing-box, based ...
The present work takes origin from studies carried out at the Department of Aerospace Engineering of...
In this work, a design strategy for optimising thin-walled structures based on a global-local finite...
Aircrafts have become one of the most important modes of travel and have grown in the recent years. ...
The paper aims to present the phases and the achievements of the aerodynamic design activities carri...
The optimization of aerospace structures is a very complex problem, owing to the hundreds of design ...
Abstract: Optimization of aerospace and lightweight structures, such as aircraft wings, is typ-icall...
This work focuses on the implementation of a complex multidisciplinary computational environment for...
The present Thesis deals with the application of optimization methods to the preliminary design of a...