Numerical micromechanical investigation of interfacial strength parameters in a carbon fibre composite material

2013 ◽  
Vol 48 (6) ◽  
pp. 749-760 ◽  
Author(s):  
DJ O'Dwyer ◽  
NP O'Dowd ◽  
CT McCarthy
Keyword(s):  
Composite Material ◽  
Carbon Fibre ◽  
Fibre Composite ◽  
Interfacial Strength ◽  
Strength Parameters ◽  
Carbon Fibre Composite ◽  
Fibre Composite Material

Tritium depth profiles in graphite and carbon fibre composite material exposed to tokamak plasmas

2001 ◽  
Vol 288 (2-3) ◽  
pp. 170-178 ◽  
Author(s):  
R.-D Penzhorn ◽  
N Bekris ◽  
U Berndt ◽  
J.P Coad ◽  
H Ziegler ◽  
...  
Keyword(s):  
Composite Material ◽  
Carbon Fibre ◽  
Fibre Composite ◽  
Tokamak Plasmas ◽  
Carbon Fibre Composite ◽  
Depth Profiles ◽  
Fibre Composite Material

Mechanical Damage to Aircraft Structures from Lightning Strikes

1993 ◽  
Vol 207 (1) ◽  
pp. 1-14 ◽  
Author(s):  
G W Reid
Keyword(s):  
Composite Material ◽  
Carbon Fibre ◽  
Fibre Composite ◽  
Mechanical Damage ◽  
Physical Damage ◽  
Carbon Fibre Composite ◽  
Fast Heating ◽  
Cross Sectional ◽  
Aircraft Structures ◽  
Lightning Strikes

The various types of current waveforms associated with lightning discharges are discussed together with their relevance to different areas of the aircraft structures. The physical damage that could be sustained by aircraft material due to lightning strikes, in particular the damage to composite material especially carbon fibre, is described. This damage is primarily due to the very fast heating and impulsive forces which lightning currents can produce. Minimum cross-sectional areas required to carry these currents safely are discussed as well as the effect of moisture content and loading the samples during test for the case of carbon fibre composite material. Details of the effects of arc attachment to various composite materials and also metal with the degree and type of damage that can be produced are reviewed.

Design and Manufacture of Recurve Bow Riser Using Fused Deposition Modeling and Fibre-Reinforced Composite Material

2015 ◽  
Vol 786 ◽  
pp. 300-304
Author(s):  
Shajahan Maidin ◽  
M.H. Jaafar
Keyword(s):  
Composite Material ◽  
Carbon Fibre ◽  
Fused Deposition Modeling ◽  
Fibre Composite ◽  
Testing Machine ◽  
Flexural Property ◽  
Carbon Fibre Composite ◽  
Fused Deposition ◽  
Final Design ◽  
Deposition Modeling

This research redesigned and manufactured the archery recurve bow riser using Fused Deposition Modeling (FDM) system to improve its design, weight and strength. Available design of bow riser was surveyed to get inspiration for new design. Final design of the bow riser design was developed with a CAD software. Prototype of the final design of the bow riser was produced by FDM system with ABS material. Coating the prototype with carbon fibre was made. Vacuum bagging process and mechanical compression process was applied to bond the multiple layers of carbon fibre composite material. The multiple layers were tested using Universal Testing Machine to test the flexural property of the redesigned carbon fibre composite coated bow riser prototype. It is found that the multiple layer of composite can withstand up to 0.1 KN of load. Thus, the study shows that reinforcing the redesigned bow riser prototype using carbon fibre composite is suitable for it is light, easy to shape and strong properties.

Carbon fibre composite development for in-ground UAV’s with NACA0012 aerofoil wing

2021 ◽  
Author(s):  
Ajanas Saludheen ◽  
Firaz Muhammed Zakariya ◽  
M Ankith ◽  
Nirmal Nandakumar ◽  
Jais George ◽  
...  
Keyword(s):  
Carbon Fibre ◽  
Fibre Composite ◽  
Carbon Fibre Composite

Hygrothermal effects on painted carbon fibre composite surfaces

2012 ◽  
Vol 47 (5) ◽  
pp. 539-547 ◽  
Author(s):  
ML de Souza ◽  
JI Mardel ◽  
BL Fox
Keyword(s):  
Carbon Fibre ◽  
Fibre Composite ◽  
Carbon Fibre Composite
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