Aeroelastic tailoring for gust load alleviation

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Abstract

This paper presents the results from the equivalent static load method applied to gust response optimisation of an aircraft wing. Through the different optimisation runs, it is assessed that gust load cases can be critical and are difficult to constrain with the sole use of static load cases. Several cases are evaluated with different gust parameters and wing boundary conditions. Effects of control efficiency and engine location are also studied.
Original languageEnglish
Title of host publicationProceedings of the 11th ASMO UK/ISSMO/NOED2016 International Conference of Numerical Optimisation Methods for Engineering Design
Subtitle of host publicationTechnische Universität München, Germany
Number of pages12
Publication statusPublished - 2016
Event11th ASMO UK/ISSMO/NOED2016 International Conference of Numerical Optimisation Methods for Engineering Design - Munich, Germany
Duration: 18 Jul 201620 Jul 2016
http://aboutflow.sems.qmul.ac.uk/events/munich2016

Conference

Conference11th ASMO UK/ISSMO/NOED2016 International Conference of Numerical Optimisation Methods for Engineering Design
Abbreviated title11th ASMO UK/ISSMO/NOED2016
CountryGermany
CityMunich
Period18/07/1620/07/16
Internet address

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