Searched for: subject%3A%22fiber%255C+metal%255C+laminates%22
(1 - 10 of 10)
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Ji, C. (author), Hu, Jiqiang (author), Alderliesten, R.C. (author), Yang, Jinchuan (author), Zhou, Zhengong (author), Sun, Yuguo (author), Wang, Bing (author)
This paper aims to illustrate the effect of the impact damage on fatigue behavior of CF/PEEK-titanium hybrid laminates. To achieve this end, a fatigue life model was proposed to predict the S–N curves of the laminates at various initial impact energy levels and stress ratios based on the energy dissipation approach. The energy dissipation...
journal article 2024
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Li, H. (author), Wang, Hao (author), Alderliesten, R.C. (author), Xiang, Junxian (author), Lin, Yanyan (author), Xu, Yingmei (author), Zhao, Haidan (author), Tao, Jie (author)
The effect of shot peen forming on the mechanical behavior of fiber metal laminates (FMLs) based on aluminium-lithium alloy was investigated to reveal the strengthening mechanism and to dispel the suspicion that shot peen forming may result in the performance deterioration of FMLs. The interlaminar, static strength and fatigue properties of...
journal article 2020
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Nardi, D. (author), Abouhamzeh, M. (author), Leonard, R.A. (author), Sinke, J. (author)
Gaps in pre-preg plies, in a case when adjacent plies do not align perfectly, may represent a significant issue in an automated fibre placement manufacturing process and can be detrimental to the properties of the final laminates. In order to tackle the consequences of gaps in the composite material, a comprehensive research has to be performed....
conference paper 2018
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Müller, B. (author), Teixeira De Freitas, S. (author), Sinke, J. (author)
The development of fiber metal laminates to multi-functional materials by embedding heater elements in the laminate extends their field of application. Fiber metal laminates with embedded heater elements are likely to be used for the de- and anti-icing of leading edges in aircraft as they combine structural and heating functions. Hence, those...
conference paper 2015
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Müller, B. (author), Teixeira de Freitas, S. (author), Sinke, J. (author)
The development of fiber metal laminates to multi-functional materials by embedding heater elements in the laminate extends their field of application. Fiber metal laminates with embedded heater elements are likely to be used for the de- and anti-icing of leading edges in aircraft as they combine structural and heating functions. Hence, those...
conference paper 2015
document
Sadighi, M. (author), Pärnänen, T. (author), Alderliesten, R.C. (author), Sayeaftabi, M. (author), Benedictus, R. (author)
The impact response of fiber metal laminates (FMLs), has been investigated with experiments and numerical simulations, which is reported in this article. Low-velocity impacts were carried out to study the effects of metal type and thickness within FMLs. Glare5-3/2 laminates with two aluminum layer thicknesses and a similar FML containing...
journal article 2012
document
Cooper, C.A. (author)
The design of complex systems in today’s aerospace domain requires a balance between the ever-increasing complexity of the supporting technology and the drive to develop those systems in a compressed timeframe. The performance knowledge of a preliminary design must shift backwards in the lifecycle in order to exploit that knowledge when there is...
doctoral thesis 2011
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De Rijck, J.J.M. (author)
The two historical fuselage failures, Comet in 1954 and Aloha in 1988, illustrate that similar accidents must be avoided which requires a profound understanding of the fatigue mechanisms involved, including analytical models to predict the fatigue behavior of riveted joints of a fuselage structure. The scope of the research project covers a...
doctoral thesis 2005
document
Verolme, J.L. (author)
doctoral thesis 1995
document
Verolme, K. (author)
report 1994
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