Determination of structural modes of vibration using digital photogrammetry

TG Ryall, CS Fraser - Journal of aircraft, 2002 - arc.aiaa.org
It is shown that it is possible to recover the three-dimensional modes of vibration of an
oscillating structure through an of ine digital photogrammetric approach employing only a …

Design studies of aeroelastic tailoring of forward-swept composite aircraft using hybrid genetic algorithm

Z Wan, C Yang, C Zou - 44th AIAA/ASME/ASCE/AHS/ASC Structures …, 2003 - arc.aiaa.org
The genetic/sensitivity-based hybrid algorithm was introduced and used for design studies
of aeroelastic tailoring of forward-swept composite aircrafts. The program of genetic …

Inverse problem of aircraft structural parameter estimation: application of neural networks

PM Trivailo, GS Dulikravich, D Sgarioto… - Inverse Problems in …, 2006 - Taylor & Francis
In this article, a novel method for estimating inertial and stiffness parameters for aircraft
structures is presented. The method is based on a combination of the finite element method …

Genetic algorithm optimisation of mathematical models using distributed computing

S Dunn, S Peucker, J Perry - Applied Intelligence, 2005 - Springer
In this paper, a process by which experimental, or historical, data are used to create
physically meaningful mathematical models is demonstrated. The procedure involves …

Advanced flutter and LCO prediction tools for flight test risk and cost reduction-an international collaborative program for T&E support

W Silva, M Brenner, J Cooper, C Denegri… - 2005 US Air Force T&E …, 2005 - arc.aiaa.org
In this paper, a TTCP+ Collaborative Program focused on the development of improved
procedures for flight flutter testing will be described. The Defense organizations of each of …

Load updating for nonlinear finite element models

J Li, RK Kapania - AIAA journal, 2007 - arc.aiaa.org
A measurement-based load updating method for finite element models subjected to static
loads was studied using a four-noded curved beam element for large displacements …

Inverse problem of aircraft structural parameter identification: application of genetic algorithms compared with artificial neural networks

PM Trivailo, T Gilbert, E Glessich… - Inverse Problems in …, 2006 - Taylor & Francis
This article is the second part of a two paper series exploring the application of two
advanced computing techniques: artificial neural networks (ANNs) and genetic algorithms …

Development of reduced order model for dynamic analysis of aircraft via global optimization

O Köse - 2023 - open.metu.edu.tr
Reduced models are often used in the early phases of aircraft design to shorten analysis
times and contribute to the optimization process. In the final stages of aircraft design …

[PDF][PDF] Indexed bibliography of genetic algorithms in materials science and engineering

JT Alander - 1994 - researchgate.net
An Indexed Bibliography of Genetic Algorithms in Materials Science and Engineering Page 1
An Indexed Bibliography of Genetic Algorithms in Materials Science and Engineering …

Genetic algorithm optimisation of mathematical models using distributed computing

S Dunn, S Peucker - … Conference on Industrial, Engineering and Other …, 2002 - Springer
In this paper, a process by which experimental, or historical, data are used to create
physically meaningful mathematical models is demonstrated. The procedure involves …