@inproceedings{4bfddc4afd9a4d99a1c8b7fa6f5626a2,
title = "Virtual aircraft model for aeroelastic simulation and load prediction of a high aspect ratio composite swept wing",
abstract = "An approach for a virtual aircraft model with the purpose to simulate the static and dynamic aeroelastic behavior of a flexible aircraft is presented. To reduce the computational effort, methods for accurate model reduction and their applicability for a flexible aircraft configuration is investigated. Static and dynamic flight maneuvers are performed to identify critical load conditions, which are furhter used with the inverse transformation for detailed structural sizing. As a computational demonstration example, a generic high aspect ratio composite aircraft swept wing is used.",
keywords = "Aircraft aeroelasticity, High AR-wing, Model reduction",
author = "Andreas Hermanutz and Mirko Hornung",
note = "Publisher Copyright: {\textcopyright} 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018. All rights reserved.; 31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018 ; Conference date: 09-09-2018 Through 14-09-2018",
year = "2018",
language = "English",
series = "31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018",
publisher = "International Council of the Aeronautical Sciences",
booktitle = "31st Congress of the International Council of the Aeronautical Sciences, ICAS 2018",
}