Assessment and Validation of Incremental Hole-Drilling Calculation Methods for Residual Stress Determination in Fiber-Metal Laminates
Author:
Funder
Deutsche Forschungsgemeinschaft
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials,Aerospace Engineering
Link
https://link.springer.com/content/pdf/10.1007/s11340-022-00848-4.pdf
Reference52 articles.
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2. Vlot A, Gunnink JW (2001) Fibre Metal Laminates. Springer Netherlands. https://doi.org/10.1007/978-94-010-0995-9
3. Roebroeks GHJJ (1994) Fibre-metal laminates: Recent developments and applications. Int J Fatigue 16(1):33–42. ISSN 0142-1123. https://doi.org/10.1016/0142-1123(94)90443-X
4. Wittenberg TC, van Baten TJ, and de Boer A (2001) Design of fiber metal laminate shear panels for ultra-high capacity aircraft. Aircr Des 4(2):99–113. ISSN 1369-8869. https://doi.org/10.1016/S1369-8869(01)00003-9
5. Botelho EC, Silva RA, Pardini LC, Rezende MC (2006) A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures. Mater Res 9:247–256. https://doi.org/10.1590/S1516-14392006000300002
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