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The effect of fiber orientation and stacking sequence on carbon/Kevlar/epoxy intraply hybrid composites under dynamic loading conditions

Samson, P. Edwin (author)
Department of Mechanical Engineering, College of Engineering, Anna University, Chennai, India
Kumaran, S. Senthil (author)
Department of Mechanical Engineering, College of Engineering, Anna University, Chennai, India
Shanmugam, Vigneshwaran (author)
Department of Mechanical Engineering, Saveetha School of Engineering, Chennai, India
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Das, Oisik (author)
Luleå tekniska universitet,Byggkonstruktion och brand
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 (creator_code:org_t)
2023-01-30
2023
English.
In: Polymers for Advanced Technologies. - : John Wiley and Sons Ltd. - 1042-7147 .- 1099-1581. ; 34:5, s. 1585-1598
  • Journal article (peer-reviewed)
Abstract Subject headings
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  • This work investigated the thermo-mechanical behavior of (carbon/Kevlar) intraply hybrid composites. The carbon/Kevlar plies' orientation and sequential arrangement were varied. Carbon and Kevlar composites, as well as five different intraply hybrids (HFRPs) composite such as carbon-0°/Kevlar-90°, carbon-45°/Kevlar-135°, carbon-90°/Kevlar-0°, carbon/Kevlar (inter-changing layer), and carbon/Kevlar-45° (inter-changing layer) composites, and a plain epoxy panel, have been developed. The thermo-mechanical characteristics of the fabricated composites were estimated using a dynamic automated analyzer under changing mechanical and thermal load conditions. The DMA technique measured the HFRPs composite visco-elastic parameters by increasing the temperature from 30°C to 150°C at frequencies ranging from 1 to 20 Hz. Flexural test characteristics for neat epoxy, carbon fiber-reinforced composites, Kevlar fiber-reinforced composites, and carbon/Kevlar fiber-reinforced composites were estimated to aid the study. The experimentally measured versus analytically calculated viscoelastic parameters were related. The results revealed that carbon-90° oriented in warp direction/Kevlar-0° oriented in weft direction exhibited higher modulus and lower loss tangent followed by carbon/Kevlar plies oriented in alternate layers and carbon/Kevlar plies oriented in inter-changing layers at 45°. Carbon-0° introduced in the weft direction/ Kevlar-90° introduced in the warp direction, and carbon-45°/Kevlar-135° exhibited intermediate storage and loss modulus and a moderate loss tangent at the various frequency levels considered in the study.

Subject headings

TEKNIK OCH TEKNOLOGIER  -- Materialteknik -- Kompositmaterial och -teknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Materials Engineering -- Composite Science and Engineering (hsv//eng)

Keyword

activation energy
dynamic mechanical analyzer
glass transition temperature
loss tangent
Byggkonstruktion
Structural Engineering

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Samson, P. Edwin
Kumaran, S. Sent ...
Shanmugam, Vigne ...
Das, Oisik
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ENGINEERING AND TECHNOLOGY
ENGINEERING AND ...
and Materials Engine ...
and Composite Scienc ...
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Polymers for Adv ...
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Luleå University of Technology

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