Impact behaviour of woven coir-epoxy composite: Effects of woven density and woven fabric treatment

Author(s):  
AR Azrin Hani ◽  
MS Hashim ◽  
TY Lim ◽  
M Mariatti ◽  
R Ahmad
2018 ◽  
Author(s):  
Pietro Russo ◽  
Giorgio Simeoli ◽  
Francesca Cimino ◽  
Maria Rosaria Ricciardi ◽  
Valentina Lopresto ◽  
...  

2004 ◽  
Vol 30 (1) ◽  
pp. 16-23
Author(s):  
Kenichi SUGIMOTO ◽  
Toshiko OSADA ◽  
Nobuyoshi KAJIOKA ◽  
Asami NAKAI ◽  
Hiroyuki HAMADA

2010 ◽  
Vol 29 (1) ◽  
pp. 14-22 ◽  
Author(s):  
N.K. Naik ◽  
P. Yernamma ◽  
N.M. Thoram ◽  
R. Gadipatri ◽  
V.R. Kavala

1993 ◽  
Vol 2 (2) ◽  
pp. 096369359300200 ◽  
Author(s):  
P Lee-Sullivan ◽  
L T Seng

The influence of stitching technique on the damage pattern of impacted glass/epoxy composite laminates was investigated. Two different techniques were evaluated; running-stitching (RS) and cross-stitching (CS) respectively. CS was found to be better than RS in suppressing delamination growth. Even so, the RS laminate was less susceptible to delamination than the unstitched equivalent. Although stitching is beneficial, it causes significant reduction in tensile stiffness but has minimal effects on the flexural modulus.


Author(s):  
Rajeev Kumar ◽  
Himanshu Pathak ◽  
Sunny Zafar

Woven fabric reinforced epoxy composite shown inherent favorable characteristics for aerospace industry applications. This paper comprehensively investigated the mechanical and fracture behavior of unidirectional carbon woven fabric reinforced epoxy composite using experimental and computational techniques. The composites were fabricated with two, four, and six ply laminates with cross-ply and inclined ply (45/–45) orientations. Laminates were fabricated using Vacuum-Assisted Resin Infusion Microwave Curing technique with a high fiber volume fraction of 50% for each laminate. Experimental analyses were performed to predict the behavior of composites under tensile, shear, and impact loading environment. Further, the mean-field homogenization technique coupled with the finite element method was employed to predict orthotropic material properties, fracture energy, and fracture parameters ( KIC and GIC) of the composite. The results showed that fracture energy obtained by the computational technique was in good agreement with experimental results. The values of GIC increased with the number of plies both for cross and inclined plies orientation composites. KIC values were higher for cross plies laminates than the inclined plies laminates.


2014 ◽  
Vol 984-985 ◽  
pp. 273-279 ◽  
Author(s):  
Chinnasamy Senthamaraikannan ◽  
S.K. Sarathkumar ◽  
Rajagopal Ramesh

Vibration damping is proving important for improved vibration control and dynamic stability in advanced engineering systems like aerospace systems, automobiles and in ship building industry. In the present investigation, vibration characteristics of woven fabric carbon composite plate reinforced with micro rubber particle blended into epoxy matrix is studied for enhancing the vibration damping performance. Test Specimens are fabricated in the form of hand layup method. CTBN rubber particle size of 5μm is selected and added to the epoxy matrix for fabricating carbon/epoxy composite plates. Rubber particles of 3% & 15 % by weight were considered as blended percentage in epoxy matrix and compared with 0% addition of rubber particles for understanding and analyzing the vibration characteristics and its difference in damping performance. Vibration damping and modal responses of various kinds of prepared plates were studied and compared. Among tested samples, carbon/epoxy composite plate with 15 wt % micro rubber particle by weight showed very good damping performance.


2011 ◽  
Vol 71 (16) ◽  
pp. 1961-1972 ◽  
Author(s):  
Mehmet Karahan ◽  
Stepan V. Lomov ◽  
Alexander E. Bogdanovich ◽  
Ignaas Verpoest

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