Load case selection technique for combined modal finite element approach of high aspect ratio wing models

A high aspect ratio wing is known to exhibit high deflection even at relatively low aerodynamic loading, making it susceptible to geometric nonlinearity. However, integrating linear and nonlinear static solutions through conventional finite element demands significant time and effort. Therefore, res...

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Bibliographic Details
Main Authors: Nordin, Norzaima, Bohari, Baizura, Chandrasegaran, Thinesh, As’arry, Azizan, Harmin, Mohammad Yazdi
Format: Article
Published: National Cheng Kung University 2023
Online Access:http://psasir.upm.edu.my/id/eprint/110079/
https://www.airitilibrary.com/Article/Detail/P20140627004-N202308290008-00003
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Institution: Universiti Putra Malaysia