K
Kin-tak Lau
Researcher at Swinburne University of Technology
Publications - 264
Citations - 15646
Kin-tak Lau is an academic researcher from Swinburne University of Technology. The author has contributed to research in topics: Epoxy & Ultimate tensile strength. The author has an hindex of 57, co-authored 260 publications receiving 12950 citations. Previous affiliations of Kin-tak Lau include Chonbuk National University & Asia University (Taiwan).
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Polylactic acid (PLA)/halloysite nanotube (HNT) composite mats: Influence of HNT content and modification
Yu Dong,Jordan Marshall,Hazim J. Haroosh,Soheila Mohammadzadehmoghadam,Dongyan Liu,Xiaowen Qi,Kin-tak Lau +6 more
TL;DR: The influence of HNT content and modification was investigated comprehensively, based on several characterisation techniques such as scanning electron microscopy (SEM), X-ray diffraction (XRD) analysis, mechanical testing, differential scanning calorimetry (DSC), thermogravimetric analysis (TGA) and Fourier transform infrared spectroscopy (FTIR).
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Effect of ultrasound sonication in nanoclay clusters of nanoclay/epoxy composites
TL;DR: In this article, the effects of ultrasound sonication in intercalated nanoclay clusters were discussed and the hardness of nanoclays/epoxy composites samples made under different sonication time was examined to compare their mechanical performances.
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Mechanical and flammability characterisations of biochar/polypropylene biocomposites
TL;DR: In this paper, the use of increasing amount of biochar to neat polypropylene continuously improved its tensile modulus and flexural strength/modulus, and the peak heat release rate and smoke production of the biocomposites were significantly reduced.
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Ternary graphene-carbon nanofibers-carbon nanotubes structure for hybrid supercapacitor
TL;DR: In this article, a hierarchical ternary carbon aerogel structure is designed by integrating graphene (Gr), carbon nanofibers (CNFs), and carbon nanotubes (CNTs).
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Use of FBG Sensors for SHM in Aerospace Structures
TL;DR: In this article, the use of the fiber Bragg grating (FBG) sensors for structural health monitoring (SHM) in aerospace fiber reinforced polymer (FRP) structures is discussed.