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Noamen Guermazi

Researcher at University of Sfax

Publications -  47
Citations -  1081

Noamen Guermazi is an academic researcher from University of Sfax. The author has contributed to research in topics: Ultimate tensile strength & Coating. The author has an hindex of 15, co-authored 45 publications receiving 798 citations. Previous affiliations of Noamen Guermazi include University of Kairouan & École Normale Supérieure.

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On the durability of FRP composites for aircraft structures in hygrothermal conditioning

TL;DR: In this article, the influence of hygrothermal conditions on p erformance of fiber-reinforced polymer (FRP) composites was investigated and the main focus of this work is to built an experimental database which may be helpful to the research and development on the design and qualification of composite repairs for aircraft structures.
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Study of UV-aging of thermoplastic polyurethane material

TL;DR: In this article, the characteristics of thermoplastic polyurethane (TPU) material exposed to artificial weathering environment for different durations were studied. And the influence on appearance and morphology, thermal properties and mechanical properties evolution of the material were investigated during aging.
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Investigations on hygrothermal aging of thermoplastic polyurethane material

TL;DR: In this article, the absorption and diffusion of water in thermoplastic polyurethane (TPU) was studied, and the effect of immersion aging on thermal, mechanical and tribological properties was given.
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Cladding of low-carbon steel to austenitic stainless steel by hot-roll bonding: Microstructure and mechanical properties before and after welding

TL;DR: In this article, the performance of cladded low-carbon steel (ASTM A283 Grade C) to austenitic stainless steel using hot-roll bonding was investigated before and after welding, and three weld samples with different configurations were prepared from cladded materials and then, these joined metals were studied.
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Investigations on the fabrication and the characterization of glass/epoxy, carbon/epoxy and hybrid composites used in the reinforcement and the repair of aeronautic structures

TL;DR: In this paper, the fabrication and characterization of glass/epoxy, carbon and hybrid laminated composites used in the reinforcement and/or the repair of aeronautic structures were discussed in terms of moisture absorption, thermal stability, tensile strength, elastic modulus, flexural strength and abrasive wear resistance.