Failure mechanisms of laminated composites subjected to static indentation

2006 ◽  
Vol 75 (1-4) ◽  
pp. 489-495 ◽  
Author(s):  
Puhui Chen ◽  
Zhen Shen ◽  
Junjie Xiong ◽  
Shengchun Yang ◽  
Shaoyun Fu ◽  
...  
1991 ◽  
pp. 669-683
Author(s):  
R. Kim ◽  
A. Miravete ◽  
S. Baselga ◽  
R. M. Bravo

2020 ◽  
Vol 245 ◽  
pp. 112327
Author(s):  
Mohamad Fotouhi ◽  
Mahdi Damghani ◽  
Mun Choong Leong ◽  
Sakineh Fotouhi ◽  
Meisam Jalalvand ◽  
...  

2021 ◽  
pp. 096739112110169
Author(s):  
Akim Djele ◽  
Ramazan Karakuzu

Nowadays, fiber reinforced laminated composites are widely used in many applications due to their high strength/weight ratio. However, these materials are very sensitive to transverse loading. The low-velocity impact test has been widely used by researchers to simulate the transverse loading. However, the low-velocity impact tests are highly toilsome, and this test requires expensive hardware and software systems. To reduce the experimental costs of the low-velocity impact test, it will be more attractive, much simpler, cheaper and more widely available to achieve impact behavior using quasi-static tests. Thus, to compare both tests, in this work the absorbed energy and force-deflection curves obtained by low-velocity impact and quasi-static indentation loading in two different fiber reinforced epoxy composites have been investigated. The Carbon-Kevlar hybrid fabrics and S2 glass fabrics were used as reinforcements. For low-velocity impact tests, a range of energies was used between 20 and 80 J. For quasi-static indentation test, the crosshead speeds were increased gradually from 1 mm/min to 60 mm/min. In addition, tests at 23°C, 40°C, 60°C and 80°C were made to examine the effect of temperature on these tests. As a result of the quasi-static tests performed, the amount of energy required to perforate the samples at a certain test speed is at the same level as the low-velocity impact test. Thus, the required energy amount for the perforation of the materials can be found by performing a quasi-static test at an appropriate speed, rather than the low-velocity impact test.


PAMM ◽  
2011 ◽  
Vol 11 (1) ◽  
pp. 251-252
Author(s):  
Christina Völlmecke ◽  
Wolfgang H. Müller

2015 ◽  
Vol 119 ◽  
pp. 693-708 ◽  
Author(s):  
M. Meng ◽  
H.R. Le ◽  
M.J. Rizvi ◽  
S.M. Grove

2015 ◽  
Vol 735 ◽  
pp. 26-30 ◽  
Author(s):  
Chi Loog Pang ◽  
Nurulakmar Abu Husain ◽  
M.R. Abdullah

Kenaf natural fibre has become the subject of interest for a wide range of engineering sectors due to its biodegradable and outstanding mechanical properties. In this study, the effect of loading rate on the indentation behaviour of fibre metal laminates (FMLs) based on kenaf/epoxy subjected to static indentation loading was investigated. The fibre metal laminates were made of chopped strand mat (CSM) kenaf fibre with epoxy resin composite and 0.6 mm thickness of 1100-O aluminium alloy sheet by using vacuum infusion process (VIP) and hydraulic pressing technique. The experiments were conducted by using a universal testing machine with loading rate of 1 mm/min, 10 mm/min and 100 mm/min. The results of indentation resistance, energy absorption and corresponding indentation failure mechanisms were compared and discussed in this study. For 2/1 FMLs, the maximum contact force increased when the loading rate increased. The loading rate did not affect the indentation failure mechanisms of the 2/1 FMLs. However, for 3/2 FMLs, delamination occurred when the specimens were indented with loading rate of 10 mm/min.


Author(s):  
Sakineh Fotouhi ◽  
Mohamad Fotouhi ◽  
Hamed Saghafi ◽  
Giangiacomo Minak ◽  
Cristiano Fragassa

The use of high strength to weight ratio laminated composites is emerging in marine industry and applications as a very efficient solution for improving productivity. Nevertheless, delamination between the layers is a limiting factor for the wider application of laminated composites, as it reduces the stiffness and strengths of the structure. Interleaving nanofibrous mats between layers of composite laminates has been proved to be an effective method for improving composites delamination resistance. This paper aims to characterize the effect of interleaved nanofiber on mode I interlaminar properties and failure mechanisms when subjected to static and fatigue loadings. For this purpose, virgin and nanomodified woven laminates were subjected to Double Cantilever Beam (DCB) specimens. Static and fatigue tests were performed and the tests were monitored by acoustic emission technique. The mechanical results showed a 130% increase of delamination toughness for nanomodified specimens in the static loadings and more crack growth resistance in the fatigue loading. The AE results revealed that different type of failure mechanisms was the cause of these improvements for the modified specimens compared with the virgin ones.


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