Low-velocity impact of rectangular foam-filled fiber metal laminate tubes
Author:
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,Mechanical Engineering,Mechanics of Materials
Link
https://link.springer.com/content/pdf/10.1007/s10483-021-2799-7.pdf
Reference27 articles.
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2. LI, H. G., XU, Y. W., HUA, X. G., LIU, C., and TAO, J. Bending failure mechanism and flexural properties of GLARE laminates with different stacking sequences. Composite Structures, 187, 354–363 (2018)
3. AMIRI, A., MOHAMMADIMEHR, M., and ANVARI, M. Stress and buckling analysis of a thick-walled micro sandwich panel with a flexible foam core and carbon nanotube reinforced composite (CNTRC) face sheets. Applied Mathematics and Mechanics (English Edition), 41(7), 1027–1038 (2020) https://doi.org/10.1007/s10483-020-2627-7
4. ZHOU, H. Y., JIA, K. C., WANG, X. J., XIONG, M. X., and WANG, Y. H. Experimental and numerical investigation of low velocity impact response of foam concrete filled auxetic honeycombs. Thin-Walled Structures, 154, 106898 (2020)
5. JING, L., LIU, K., SU, X. Y., and GUO, X. Experimental and numerical study of square sandwich panels with layered-gradient foam cores to air-blast loading. Thin-Walled Structures, 161, 107445 (2021)
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4. Analytical and Numerical Investigation on Dynamic Behavior of Rectangular FML Sandwich Tubes with Metal Foam Core Under Low-Velocity Impact;International Journal of Applied Mechanics;2022-05
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