Results 21 to 30 of about 13,057 (258)

Effect of compression and tension types of concentrated edge loads on buckling and vibration behavior of interlaminar hybrid fibre metal laminates

open access: yesComposites Part C: Open Access, 2021
The present study deals with the numerical investigation on the buckling and vibration behaviour of interlayer hybrid fibre metal laminates (HFMLs) subjected to different types of concentrated edge compression and tension loads.
P.P. Yathish Muddappa   +2 more
doaj   +1 more source

Measuring the notched compressive strength of composite laminates: Specimen size effects [PDF]

open access: yes, 2008
Large fibre reinforced composite structures can give much lower strengths than small test specimens, so a proper understanding of scaling is vital for their safe and efficient use.
C. Soutis   +15 more
core   +3 more sources

Evaluation of Force-Time Changes During Impact of Hybrid Laminates Made of Titanium and Fibrous Composite

open access: yesArchives of Metallurgy and Materials, 2016
Fibre metal laminates (FML) are the modern hybrid materials with potential wide range of applications in aerospace technology due to their excellent mechanical properties (particularly fatigue strength, resistance to impacts) and also excellent corrosion
Jakubczak P., Surowska B., Bieniaś J.
doaj   +1 more source

Mechanical Properties of Thermoplastic-Based Hybrid Laminates with Regard to Layer Structure and Metal Volume Content

open access: yesMetals, 2020
Multi layered lightweight material compounds such as hybrid laminates are composed of different layers of materials like metals and unidirectional fibre-reinforced plastics and offer high specific strength.
Maik Trautmann   +3 more
doaj   +1 more source

A review on forming technologies of fibre metal laminates

open access: yesInternational Journal of Lightweight Materials and Manufacture, 2021
Fibre metal laminates (FMLs), as a class of hybrid material taking advantages of both metals and composites, have shown great promise as lightweight structural materials in the transportation industry.
Zerong Ding   +3 more
doaj   +1 more source

Numerical Shear Buckling Investigation of GLAREs with Initial Delamination

open access: yesAdvances in Materials Science and Engineering, 2022
GLAREs as hybrid materials are widely employed members of fibre metal laminates (FMLs) in aerospace structures. Delamination is one of the most critical failure modes that happen during the manufacturing or service life, decreasing the stability and ...
Maryam Niazi, Mohammad Homayoune Sadr
doaj   +1 more source

A brief review of modified conductive carbon/glass fibre reinforced composites for structural applications: Lightning strike protection, electromagnetic shielding, and strain sensing

open access: yesComposites Part C: Open Access, 2021
Multi-functional fibre-reinforced polymer (FRP) laminates are the requirements of advanced aircraft structures. FRP laminates are the primary design to carry structural loads.
S. Das, T. Yokozeki
doaj   +1 more source

Influence of woven ply degradation on fatigue crack growth in thin notched composites under tensile loading [PDF]

open access: yes, 2010
This paper deals with the fatigue of the through the-thickness crack propagation in thin notched composite laminates made of two glass woven plies. It highlights the different crack growths between warp and weft directions of the woven ply.
Barrau, Jean-Jacques   +3 more
core   +3 more sources

Energy absorption and bending stiffness in CFRP laminates : the effect of 45º plies [PDF]

open access: yes, 2008
The impact characteristics of cross-ply and angle-ply composite laminates were investigated, with an instrumented impact drop tester by performing gravity assisted drop tests on [0/90]6s and [0/45/90]4s laminates.
Alexander, N.V.   +3 more
core   +1 more source

Analysis on drilling of woven glass fibre reinforced aluminium sandwich laminates

open access: yesJournal of Materials Research and Technology, 2019
Fibre metal laminates being used in aerospace industries becomes primary composite material under research, since its application finds on the outer covering of the fuselage skin structure, the holes are need to be drilled on it, to assemble it.
Gopalakrishnan Ramya Devi   +1 more
doaj   +1 more source

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