Impact resistance of fiber-metal laminates: A review

被引：290
作者：
Sadighi, M. [1 ]
Alderliesten, R. C. [2 ]
Benedictus, R. [2 ]
机构：
[1] Amirkabir Univ Technol, Dept Mech Engn, Tehran, Iran
[2] Delft Univ Technol, Fac Aerosp Engn, Struct & Mat Lab, NL-2600 GB Delft, Netherlands
来源：
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING | 2012年 / 49卷
关键词：
Fiber metal laminates; Impact; Low/high velocity; Experimental; Theoretical; MECHANICAL-BEHAVIOR; PART; FRACTURE PROPERTIES; DAMAGE TOLERANCE; COMPOSITE; ALUMINUM; FAILURE; SIMULATION; PREDICTION; FATIGUE;
D O I：
10.1016/j.ijimpeng.2012.05.006
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
Combining the suitable properties of metals and fiber reinforced composites, as the idea behind the application of new types of materials, called fiber metal laminates (FMLs), have lead to superior impact properties as well as considerable improvement in fatigue performance. The characteristics of FMLs under impact loading and the ways to improve their properties to withstand this type of loading could be of particular importance in aerospace structures and other applications. This paper reviews relevant literature which deals with experimental evidence of "material related" and "event related" impact resistance parameters as well as the articles related to theoretical and numerical simulation of impact loading of FMLs. Relevant results will be discussed and the recommendations that need to be resolved in the future will be addressed. (C) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码：77 / 90
页数：14
相关论文
共 96 条
[1]  
Abatan A, 2002, J THERMOPLAST COMPOS, V15, P375, DOI [10.1177/0892705702015005732, 10.1106/089270502022732]
[2]   The impact resistance of polypropylene-based fibre-metal laminates [J].
Abdullah, M. R. ;
Cantwell, W. J. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (11-12) :1682-1693
[3]  
Abrate Serge., 1998, IMPACT COMPOSITE STR, DOI 10.1017/CBO9780511574504
[4]   On the fracture mechanical behaviour of fibre reinforced metal laminates (FRMLs) [J].
Afaghi-Khatibi, A ;
Lawcock, G ;
Ye, L ;
Mai, YW .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2000, 185 (2-4) :173-190
[5]  
Alderliesten Rene, 2009, Recent Patents on Engineering, V3, P25, DOI 10.2174/187221209787259893
[6]   Fatigue and damage tolerance of Glare [J].
Alderliesten, RC ;
Hagenbeek, M ;
Homan, JJ ;
Hooijmeijer, PA ;
De Vries, TJ ;
Vermeeren, CAJR .
APPLIED COMPOSITE MATERIALS, 2003, 10 (4-5) :223-242
[7]   The applicability of magnesium based Fibre Metal Laminates in aerospace structures [J].
Alderliesten, Rene ;
Rans, Calvin ;
Benedictus, Rinze .
COMPOSITES SCIENCE AND TECHNOLOGY, 2008, 68 (14) :2983-2993
[8]   An experimental investigation on the impact response of fiberglass/aluminum composites [J].
Atas, Cesim .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2007, 26 (14) :1479-1491
[9]   The response of aluminium/GLARE hybrid materials to impact and to in-plane fatigue [J].
Bagnoli, F. ;
Bernabei, M. ;
Figueroa-Gordon, D. ;
Irving, P. E. .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2009, 523 (1-2) :118-124
[10]  
Benedictus, 2007, 48 AIAA ASME ASCE AH, P1
12345678910