[1] Darab S, Pol MH, Rahi A. Experimental Investigation of Aluminum Foam Sandwich Panels under Quasi-static Loading. Iranian Journal of Manufacturing Engineering. 2020 Sep 22;7(7):14-23. [In Persian]
[2] Zhang Y, Li Y, Guo K, Zhu L. Dynamic mechanical behaviour and energy absorption of aluminium honeycomb sandwich panels under repeated impact loads. Ocean Engineering. 2021 Jan 1;219:108344.
doi: 10.1016/j.oceaneng.2020.108344
[3] Mahmoudabadi MZ, Sadighi M. Experimental investigation on the energy absorption characteristics of honeycomb sandwich panels under quasi-static punch loading. Aerospace Science and Technology. 2019 May 1;88:273-86.
doi: 10.1016/j.ast.2019.02.035
[4] Khaire N, Tiwari G, Patel V, Iqbal MA. Assessment of the ballistic response of honeycomb sandwich structures subjected to offset and normal impact. Defence Technology. 2023 Oct 1;28:56-73.
doi: 10.1016/j.dt.2022.12.018
[5] Tariq F, Uzair M, Shifa M. Residual compressive strength of aluminum alloy honeycomb sandwich panel in the presence of multiple impact dents. Journal of Sandwich Structures & Materials. 2022 Feb;24(2):1189-205.
doi: 10.1177/10996362211036987
[6] Sun G, Chen D, Wang H, Hazell PJ, Li Q. High-velocity impact behaviour of aluminium honeycomb sandwich panels with different structural configurations. International Journal of Impact Engineering. 2018 Dec 1;122:119-36.
doi: 10.1016/j.ijimpeng.2018.08.007
[7] Zhang Y, Yan L, Zhang C, Guo S. Low-velocity impact response of tube-reinforced honeycomb sandwich structure. Thin-Walled Structures. 2021 Jan 1;158:107188.
doi: 10.1016/j.tws.2020.107188
[8] Petras A, Sutcliffe MP. Failure mode maps for honeycomb sandwich panels. Composite structures. 1999 Apr 1;44(4):237-52.
doi: 10.1016/S0263-8223(98)00123-8
[9] Foo CC, Seah LK, Chai GB. Low-velocity impact failure of aluminium honeycomb sandwich panels. Composite structures. 2008 Sep 1;85(1):20-8.
doi: 10.1016/j.compstruct.2007.10.016
[10] Crupi V, Epasto G, Guglielmino E. Collapse modes in aluminium honeycomb sandwich panels under bending and impact loading. International Journal of Impact Engineering. 2012 May 1;43:6-15.
doi: 10.1016/j.ijimpeng.2011.12.002
[11] Zhang X, Xu F, Zang Y, Feng W. Experimental and numerical investigation on damage behavior of honeycomb sandwich panel subjected to low-velocity impact. Composite Structures. 2020 Mar 15;236:111882.
doi: 10.1016/j.compstruct.2020.111882
[12] Sun G, Huo X, Wang H, Hazell PJ, Li Q. On the structural parameters of honeycomb-core sandwich panels against low-velocity impact. Composites Part B: Engineering. 2021 Jul 1;216:108881.
doi: 10.1016/j.compositesb.2021.108881
[13] Hassanpour Roudbeneh F, Liaghat G, Sabouri H, Hadavinia H. Experimental investigation of quasistatic penetration tests on honeycomb sandwich panels filled with polymer foam. Mechanics of advanced materials and Structures. 2020 Nov 2;27(21):1803-15.
doi: 10.1080/15376494.2018.1525628
[14] Rezayat HR, Toozandehjani H, Zakeri A. Experimental study of energy absorption of sandwich panel with composite/elastomer skin. Iranian Journal of Manufacturing Engineering. 2023 Dec 22;10(10):26-42.
doi: 10.22034/IJME.2023.418015.1840 [In Persian]
[15] Military standard Sandwich Constructions and core materials, MIL-STD-410B, General test method, Department of Defens, Washington, D.C. 1967.
[16] Military standard adhesive film form Sandwich Constructions, MIL-A-25463.Department of Defens, Washington, D.C.1982.
[17] Zhu S, Chai GB. Damage and failure mode maps of composite sandwich panel subjected to quasi-static indentation and low velocity impact. Composite structures. 2013 Jul 1;101:204-14.
doi: 10.1016/j.compstruct.2013.02.010
