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 language | English |
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Title of host publication | Proceedings of the 11th ASMO UK/ISSMO/NOED2016 International Conference of Numerical Optimisation Methods for Engineering Design |
Subtitle of host publication | Technische Universität München, Germany |
Number of pages | 12 |
Publication status | Published - 2016 |
Event | 11th ASMO UK/ISSMO/NOED2016 International Conference of Numerical Optimisation Methods for Engineering Design - Munich, Germany Duration: 18 Jul 2016 → 20 Jul 2016 http://aboutflow.sems.qmul.ac.uk/events/munich2016 |
Conference
Conference | 11th ASMO UK/ISSMO/NOED2016 International Conference of Numerical Optimisation Methods for Engineering Design |
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Abbreviated title | 11th ASMO UK/ISSMO/NOED2016 |
Country/Territory | Germany |
City | Munich |
Period | 18/07/16 → 20/07/16 |
Internet address |