Results 241 to 250 of about 1,465 (303)

Characterization of progressive damage behaviour and failure mechanism of carbon fiber reinforced composite laminates. [PDF]

Sci Rep
Liu Y, Xie J, Chen X, Zhang J, Wan M, Sun Z, Yang C.   +6 more
europepmc   +1 more source

Analysis of Thermally Induced Residual Stress in Resistance Welded PC/CF Composite to Aluminum. [PDF]

Materials (Basel)
Praski M, Kowalczyk P, Stankiewicz K, Szumowski R, Synaszko P, Leski A.   +5 more
europepmc   +1 more source

Stochastic Finite Element Modelling of Fibre-Metal Laminates [PDF]

45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference, 2004
Fibre-metal laminates are expected to have larger variations in material properties compared to traditional aerospace materials such as aluminium. Eects of such variations are not taken into account in current numerical models. This paper discusses the development of a stochastic nite element model with the existing deterministic solidlike shell (SLS ...
Chung, D.B., Gutierrez de La Merced, M.A., Remmers, J.J.C., de Borst, René   +3 more
openaire   +3 more sources

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Fatigue initiation in fibre metal laminates

International Journal of Fatigue, 2006
Abstract It is assumed that fatigue crack initiation in Fibre Metal Laminates is determined by the stress cycles in the metal layers only. It is further assumed that if the stress cycles in the metal layers are known, the fatigue initiation life can be established using S – N data available for the given metal alloy.
exaly   +2 more sources

The meaning of threshold fatigue in fibre metal laminates

International Journal of Fatigue, 2009
This paper discusses the meaning of threshold fatigue for fibre metal laminates under constant amplitude loading. A few experiments have been performed and the results are discussed in this paper.
René Alderliesten, Calvin Rans
exaly   +2 more sources

Delamination buckling of fibre–metal laminates

Composites Science and Technology, 2001
A fibre–metal laminate is a composite of metal and fibre-reinforced prepreg layers. An example of such a material is Glare. It consists of alternating layers of aluminium and glass-fibre-reinforced prepreg. The material can be sensitive to delamination buckling, which occurs when a partially delaminated panel is subjected to a compressive force.
Remmers, J.J.C., Borst, de, R.
openaire   +2 more sources

Multiscale analyses of fibre metal laminates [PDF]

, 2008
Aerospace ...
Cid Alfaro, M.V. (author), Cid Alfaro, M.V.   +1 more
openaire   +2 more sources

Recycling of aluminum from fibre metal laminates

Journal of Shanghai Jiaotong University (Science), 2012
Recycling of aluminum alloy scrap obtained from delaminated fibre metal laminates (FMLs) was studied through high temperature refining in the presence of a salt flux. The aluminum alloy scrap contains approximately mass fraction w(Cu) = 4.4%, w(Mg) = 1.1% and w(Mn) = 0.6% (2024 aluminum alloy).
Zhu, G. (author), Xiao, Y. (author), Yang, Y. (author), Wang, J. (author), Sun, B. (author), Boom, R. (author)   +5 more
openaire   +3 more sources