Analysis Prediction and Correlation of Fiber Metal Laminate Crack Growth in Semi-Wing Full-Scale Test
Analysis Prediction and Correlation of Fiber Metal Laminate Crack Growth in Semi-Wing Full-Scale Test
- Neue Suche nach: Mendonça, Willy R. P.
- Neue Suche nach: Silva, Danielle F. N. R.
- Neue Suche nach: Mendonça, Willy R. P.
- Neue Suche nach: Silva, Danielle F. N. R.
Abstract This paper aims to demonstrate the correlation between simulation and experimental results obtained for artificially inserted crack propagation in the Full-Scale fatigue test of a semi-wing, developed by Embraer. The cracks were inserted on the lower wing skin, which was manufactured in Fiber Metal Laminates (FML), in order to validate the analysis methodology in this material. The application of cracks in a Full-scale test allowed the evaluation of several damage scenarios that could hardly be reproduced with high fidelity in panel tests, by incorporating: design details without simplifications and load redistribution among structural components. The analysis and test results will be substantiated and discussed.
Dokumentinformationen
Analysis Prediction and Correlation of Fiber Metal Laminate Crack Growth in Semi-Wing Full-Scale Test
2019-07-03
13 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Ähnliche Titel
Validation of Crack Growth Analysis Technique for a Fiber Metal Laminate (AIAA 2014-1382)
| British Library Conference Proceedings | 2014
Crack growth behavior of internal titanium plies of a fiber metal laminate
| Tema Archiv | 2008
AIRCRAFT WING AND FIBER METAL LAMINATE FORMING PART OF SUCH AN AIRCRAFT WING
| Europäisches Patentamt | 2018
Aircraft wing and fiber metal laminate forming part of such an aircraft wing
| Europäisches Patentamt | 2017