Experimental study on stress attenuation in aluminum foam core sandwich panels in high-velocity impact

被引:16
|
作者
Liang, Xiaolong [1 ]
Luo, Hongjie [1 ,2 ]
Mu, Yongliang [1 ,2 ]
Wu, Linli [1 ,2 ]
Lin, Hao [1 ]
机构
[1] Northeastern Univ, Sch Met, Shenyang 110819, Peoples R China
[2] Minist Educ Mat Adv Preparat, Engn Technol Res Ctr, Shenyang 110819, Peoples R China
基金
中国国家自然科学基金;
关键词
Metallic composites; Porous materials; High-velocity impact; PVDF transducer; Stress attenuation; Damage profile; AIR BLAST; HONEYCOMBS; BEHAVIOR; ARMOR;
D O I
10.1016/j.matlet.2017.05.036
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The present work examined the dynamic behaviors of sandwich panels with aluminum foam core and steel faceplates at an impact velocity of about 370 m/s. The stress attenuation before and after the foam core during penetration process was measured by means of Polyvinylidene Fluoride transducers. It was found that the stress value was remarkably reduced, and the rise velocity of stress slowed down evidently as foam core was compressed. The profile of the damaged aluminum foam illustrated no obvious localized "X" failure patterns at the velocity tested presently. (C) 2017 Elsevier B.V. All rights reserved.
引用
收藏
页码:100 / 102
页数:3
相关论文
共 50 条
  • [41] Ballistic Resistance of Honeycomb Sandwich Panels under In-Plane High-Velocity Impact
    Qi, Chang
    Yang, Shu
    Wang, Dong
    Yang, Li-Jun
    SCIENTIFIC WORLD JOURNAL, 2013,
  • [42] High-velocity impact behaviour of aluminium honeycomb sandwich panels with different structural configurations
    Sun, Guangyong
    Chen, Dongdong
    Wang, Hongxu
    Hazell, Paul J.
    Li, Qing
    INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2018, 122 : 119 - 136
  • [43] A new method for the study of parabolic impact of foam-core sandwich panels
    Ramakrishnan, Karthik Ram
    Guerard, Sandra
    Maheo, Laurent
    Shankar, Krishna
    Viot, Philippe
    COMPOSITES PART B-ENGINEERING, 2019, 167 : 717 - 727
  • [44] Low velocity bending impact behavior of foam core sandwich beams: Experimental
    Caliskan, Umut
    Apalak, M. Kemal
    COMPOSITES PART B-ENGINEERING, 2017, 112 : 158 - 175
  • [45] Low velocity failure and integrity assessment of foam core sandwich panels
    Mocian, Oana Alexandra
    Constantinescu, Dan Mihai
    Sorohan, Stefan
    Sandu, Marin
    FRATTURA ED INTEGRITA STRUTTURALE, 2019, 13 (48): : 230 - 241
  • [46] Study on the Compressive Behavior of the Aluminum Foam Sandwich Panels
    Wang, Zhiguo
    Zhao, Weimin
    Qin, Chunling
    Ding, Jian
    Xia, Xingchuan
    Wei, Zhihao
    POROUS METALS AND METALLIC FOAMS, METFOAM 2011, 2012, : 541 - 546
  • [47] Experimental research on damage characteristics of CFRP/aluminum foam sandwich structure subjected to high velocity impact
    Tang, Enling
    Zhang, Xiaoqi
    Han, Yafei
    JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T, 2019, 8 (05): : 4620 - 4630
  • [48] Impact response of aluminum corrugated core sandwich panels
    Wadley, H. N. G.
    Dharmasena, K. P.
    O'Masta, M. R.
    Wetzel, J. J.
    INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2013, 62 : 114 - 128
  • [49] High-velocity impact behaviour of damaged sandwich plates with agglomerated cork core
    Ivanez, I.
    Sanchez-Saez, S.
    Garcia-Castillo, S. K.
    Barbero, E.
    Amaro, A.
    Reis, P. N. B.
    COMPOSITE STRUCTURES, 2020, 248
  • [50] High-velocity impact experiment of aluminum foam sample using powder gun
    Tanaka, Shigeru
    Hokamoto, Kazuyuki
    Irie, Seiichi
    Okano, Toshihiko
    Ren, Zoran
    Vesenjak, Matej
    Itoh, Shigeru
    MEASUREMENT, 2011, 44 (10) : 2185 - 2189