Numerical Analysis of Flat Panel Composite Material for Two-Bay Crack Arrest Competency with Fractured Central Longeron
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Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s40033-024-00663-2.pdf
Reference35 articles.
1. S. Shroff, E. Acar, C. Kassapoglou, Design, analysis, fabrication, and testing of composite grid-stiffened panels for aircraft structures. Thin-Walled Structures 119, 235–246 (2017)
2. Ucan, Hakan, Hilmar Apmann, Gregor Graßl, Christian Krombholz, Kai Fortkamp, Dorothea Nieberl, Fabian Schmick, Chinh Nguyen, and D. Akin. "Production technologies for lightweight structures made from fibre–metal laminates in aircraft fuselages." CEAS Aeronautical Journal 10, no. 2 (2019): 479–489.
3. Mukhopadhyay, Vivekanand, Jason Welstead, Jesse Quinlan, and Mark D. Guynn. "Structural Configuration Systems Analysis for Advanced Aircraft Fuselage Concepts." In AIAA Modeling and Simulation Technologies Conference, p. 4419. 2016.
4. Branco, Ricardo, F. V. Antunes, and J. D. Costa. "A review on 3D-FE adaptive remeshing techniques for crack growth modelling." Engineering Fracture Mechanics 141 (2015): 170–195.
5. D. Simunek, M. Leitner, J. Maierhofer, H.-P. Gänser, R. Pippan, Analytical and numerical crack growth analysis of 1: 3 scaled railway axle specimens. Metals 9(2), 184 (2019)
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