Abstract
This paper describes testing and analysis performed on integrally stiffened aluminum panels reinforced by carbon-epoxy or boron-epoxy bonded strips. Testing was performed at roomtemperature and at -50°C. The test results identify a large potential for increasing significantly the damage-tolerance life of these panels. The analytical results, based on finite-element models, correlate very well with the test results. © Springer Science+Business Media B.V. 2009.
Cite
CITATION STYLE
Brot, A., Peleg-Wolfin, Y., Kressel, I., & Yosef, Z. (2009). The use of composite material strips to extend the damage-tolerance life of integrally stiffened aluminum panels. In ICAF 2009, Bridging the Gap Between Theory and Operational Practice - Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue (pp. 237–244). Kluwer Academic Publishers. https://doi.org/10.1007/978-90-481-2746-7_14
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