This presentation has been held at the "Practicalities of Analysing Composite Materials" seminar in Coventry, UK on the 5th of December, 2023.
Traditional structural design methods in Aeronautics explore a very large number of design variables using simple models, suitably calibrated following decades of experience, as well as extensive experimental and simulation data. More detailed finite element models are finally created to verify the design, but only once the design space has been very significantly reduced, and vast aspects of the design have been fixed. This process creates an obvious problem when moving away from the design space for which the simple models used at the start of this process were calibrated. A possible solution to the above consists of detailed finite element models of very large aircraft structures that have the capability to represent the detail required to predict likely hotspots in structural components such as a wing, and where the discretisation and the design variables can evolve during the analysis as required. Possible approaches for achieving such models will be presented during the talk.
Reference | comp23-04 |
---|---|
Authors | Costa. R. O. S. S. Matos. M |
Language | English |
Audiences | Analyst Manager |
Type | Presentation |
Date | 5th December 2023 |
Organisation | Imperial College London |
Region | UK |
Stay up to date with our technology updates, events, special offers, news, publications and training
If you want to find out more about NAFEMS and how membership can benefit your organisation, please click below.
Joining NAFEMS© NAFEMS Ltd 2024
Developed By Duo Web Design