This master thesis work presents the development of a parameterized automated generic model for the structural design of an aircraft wing. Furthermore, in order to perform finite element analysis on the aircraft wing geometry, the process of finite element mesh generation is automated. Aircraft conceptual design is inherently a multi-disciplinary design process which involves a large number of disciplines and expertise. In this thesis work, it is investigated how high-end CAD software‟s can be used in the early stages of an aircraft design process, especially for the design of an aircraft wing and its structural entities wing spars and wing ribs. The generic model that is developed in this regard is able to automate the process of creation ...
This project details the structural analysis of the wings of two Radio-controlled aircraft, designed...
Purpose – To obtain a good start configuration in the early design phase, simulation tools are used ...
The design process of new air- and rotorcraft is commonly separated into three different consecutive...
Abstract This work presents the development of a parameterized automated generic model for the struc...
In the present work, a code for parametric automated generation of Finite Element (FE) models for th...
Aircraft structural layout concept design at Saab Aeronautics utilize thickness optimizationto evalu...
Aircraft structural layout concept design at Saab Aeronautics utilize thickness optimizationto evalu...
The paper presents a comprehensive parameterization concept to set up complex structural models for ...
Summarization: In this work a surface generation software named Ge.P.A.S. (for generic parameterized...
AbstractA finite element parametric modeling method of aircraft wing structures is proposed in this ...
This article introduces a high-fidelity geometry definition methodology enabling Multidisciplinary D...
This article introduces a high-fidelity geometry definition methodology enabling Multidisciplinary D...
The development of new air- and rotorcraft is very challenging. The design process is divided into t...
The product development cycles in all sectors of the industry become shorter. Simultaneously, the pe...
This paper introduces a fully parameterized finite element based tool chain for the structural sizin...
This project details the structural analysis of the wings of two Radio-controlled aircraft, designed...
Purpose – To obtain a good start configuration in the early design phase, simulation tools are used ...
The design process of new air- and rotorcraft is commonly separated into three different consecutive...
Abstract This work presents the development of a parameterized automated generic model for the struc...
In the present work, a code for parametric automated generation of Finite Element (FE) models for th...
Aircraft structural layout concept design at Saab Aeronautics utilize thickness optimizationto evalu...
Aircraft structural layout concept design at Saab Aeronautics utilize thickness optimizationto evalu...
The paper presents a comprehensive parameterization concept to set up complex structural models for ...
Summarization: In this work a surface generation software named Ge.P.A.S. (for generic parameterized...
AbstractA finite element parametric modeling method of aircraft wing structures is proposed in this ...
This article introduces a high-fidelity geometry definition methodology enabling Multidisciplinary D...
This article introduces a high-fidelity geometry definition methodology enabling Multidisciplinary D...
The development of new air- and rotorcraft is very challenging. The design process is divided into t...
The product development cycles in all sectors of the industry become shorter. Simultaneously, the pe...
This paper introduces a fully parameterized finite element based tool chain for the structural sizin...
This project details the structural analysis of the wings of two Radio-controlled aircraft, designed...
Purpose – To obtain a good start configuration in the early design phase, simulation tools are used ...
The design process of new air- and rotorcraft is commonly separated into three different consecutive...