Aeroelastic tailoring for gust load alleviation

Title

Aeroelastic tailoring for gust load alleviation

 Author

Lancelot, P.M.G.J. (TU Delft Aerospace Structures & Computational Mechanics) ORCID 0000-0002-4833-2405
De Breuker, R. (TU Delft Aerospace Structures & Computational Mechanics) ORCID 0000-0002-7882-2173

 Date

2016

 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.

 To reference this document use:

http://resolver.tudelft.nl/uuid:4798d555-69ca-472a-9bd4-9d050fd71c90

 Source

Proceedings of the 11th ASMO UK/ISSMO/NOED2016 International Conference of Numerical Optimisation Methods for Engineering Design: Technische Universität München, Germany

 Event

11th ASMO UK/ISSMO/NOED2016 International Conference of Numerical Optimisation Methods for Engineering Design, 2016-07-18 → 2016-07-20, Munich, Germany

 Part of collection

Institutional Repository

 Document type

conference paper

 Rights

© 2016 P.M.G.J. Lancelot, R. De Breuker
Files
PDF Paper_NOED_2016_Lancelot_ ... reuker.pdf 1.15 MB
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