References
[1]. Chai, G. B., & Zhu, S. (2011). A review of low-velocity
impact on sandwich structures. Proceedings of the
Institution of Mechanical Engineers, Part L: Journal of
Materials: Design and Applications, 225(4), 207-230.
[2]. Dikshit, V., Prasanth, N. A., Kumar, J. D., Yap, Y. L., & Yeong, W. Y. (2016). Investigation of quasi static indentation on 3D printed honeycomb based truncated- pyramid square structure. Proceedings of the 2nd International Conference on Progress in Additive Manufacturing (Pro-AM 2016), 116-121.
[3]. Flores-Johnson, E. A., & Li, Q. M. (2010). Indentation
into polymeric foams. International Journal of Solids and
Structures, 47(16), 1987-1995.
[4]. Flores-Johnson, E. A., & Li, Q. M. (2011). Experimental
study of the indentation of sandwich panels with carbon
fibre-reinforced polymer face sheets and polymeric foam
core. Composites Part B: Engineering, 42(5), 1212-1219.
[5]. Flores-Johnson, E. A., Li, Q. M., & Shen, L. (2014).
Numerical simulations of quasi-static indentation and low
velocity impact of Rohacell 51 WF foam. International
Journal of Computational Methods, 11, 1344004.
[6]. Li, Y., Xuefeng, A., & Xiaosu, Y. (2012). Comparison
with Low-Velocity Impact and Quasi-staticIndentation
Testing of Foam Core Sandwich Composites. International Journal of Applied Physics and
Mathematics, 2(1), 58.
[7]. Li, Z., Zheng, Z., Yu, J., & Yang, J. (2014). Indentation of
composite sandwich panels with aluminum foam core:
An experimental parametric study. Journal of Reinforced
Plastics and Composites, 33(18), 1671-1681.
[8]. Lie, S. C. (1989). Damage resistance and damage
tolerance of thin composite facesheet honeycomb
panels (Doctoral Dissertation, Massachusetts Institute of
Technology).
[9]. Luo, L., Zhang, Z., Li, M., Shen, Z., & Yang, S. (2007).
Experimental study on quasi-static indentation damage
resistance of composite laminates. Fuhe Cailiao Xuebao
(Acta Mater. Compos. Sin.), 24(3), 154-159.
[10]. Proulx, T. (Ed.). (2011). Experimental and Applied
Mechanics, Volume 6. Proceedings of the 2010 Annual
Conference on Experimental and Applied Mechanics
(Vol. 17). Springer Science & Business Media.
[11]. Ruan, D., Lu, G., & Wong, Y. C. (2010). Quasi-static
indentation tests on aluminium foam sandwich panels.
Composite Structures, 92(9), 2039-2046.
[12]. Sharma, R. S., Raghupathy, V. P., Priyamvada, G. M.,
Abishek, A., & Abhiraj, M. (2011). Investigation of Low
Velocity Impact Response of Aluminum Honeycomb
Sandwich Panels. ARPN Journal of Engineering and
Applied Sciences, 6(11), 7-4.
[13]. Shen, Z., Yang, S. C., & Chen, P. H. (2007). Behaviors
of composite materials to withstand impact and structural
compressive design allowableness. Acta Aeronautica et
Astronautica Sinica- Series A and B, 28(3), 561.
[14]. Shen, Z., Zhang, Z. L., & Wang, J. (2004).
Characterization of damage resistance and damage
tolerance behaviour of composite laminates. Fuhe
Cailiao Xuebao/Acta Materiae Compositae Sinica,
21(5), 140–145.
[15]. Steeves, C. A., & Fleck, N. A. (2004). Material
selection in sandwich beam construction. Scripta
Materialia, 50(10), 1335-1339.
[16]. Steinmann, A. E. (1977). Damage Tolerance of Thin
Skin Sandwich Panels (No. AFML-TR-76-185). Air Force
Materials Lab Wright-Patterson AFB Ohio.
[17]. Tsang, P. H. W. (1994). Impact resistance and
damage tolerance of composite sandwich panels
(Doctoral Dissertation, Massachusetts Institute of
Technology).
[18]. Wang, X., Peng, X., & Guo, Z. (2014). An
experimental study of the indentation behaviour of Al
foam. Engineering Review, 34(1), 15-21.
[19]. Xia, F., & Wu, X. (2010). Work on low-velocity impact
properties of foam sandwich composites with various
face sheets. Journal of Reinforced Plastics and
Composites, 29(7), 1045-1054.
[20]. Zhang, F., Mohmmed, R., Sun, B., & Gu, B. (2013).
Damage Behaviors of Foam Sandwiched Composite
Materials Under Quasi-Static Three-point Bending. Applied
Composite Materials, 20(6), 1231-1246.
