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Akademický článek

A comparative study of propagation delay applied on varieties carbon nanotubes Bundles interconnects using the FDTD and the ABCD matrix method

Autor: Nadir Youssef, Belahrach Hassan, Ghammaz Abdelilah, Naamane Aze-eddine, Radouani Mohammed

Publikováno v: ITM Web of Conferences, Vol 52, p 04001 (2023)

Due to their hilarious properties, carbon nanotubes (CNTs) with their different varieties have been suggested as potential alternatives for interconnects in many industrial applications related to Artificial Intelligence. This work made an overview o

Externí odkaz: https://doaj.org/article/ab9d15259a694975ace721296f17e8e4

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Akademický článek

Optimization study of the cementitious matrix for the confinement of radioactive ion exchange resins: preparation and characterization

Autor: Sadiq Asmae, Moukrim Nihal, Naamane Ayoub, Faiz Zineb, El Ghailassi Touria, Bouih Abderahim, Hannache Hassan, Fakhi Said

Publikováno v: ITM Web of Conferences, Vol 43, p 01026 (2022)

In order to optimize the formulation of the conditioning matrix of the Ion Exchange Resins (IER) (MBD-15), considered as radioactive waste generated by the TRIGA MARK II nuclear reactor of the CENM, we carried out several tests by fixing the percenta

Externí odkaz: https://doaj.org/article/3811fdea4986411281557f22dc7e87bd

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The Acquisition of Semantic Relationships between words

Autor: Naamane, Mohamed

The study of semantic relationships has revealed a close connection between these relationships and the morphological characteristics of a language. Morphology, as a subfield of linguistics, investigates the internal structure and formation of words.

Externí odkaz: http://arxiv.org/abs/2307.06419

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Design of F-16 Airfoil Mock-ups for Supersonic Wind Tunnel: Study, Production, Testing and Validation

Autor: Eddegdag, N., Naamane, A., Radouani, M., Gadari, M. El

This research paper presents a comprehensive investigation into the behavior of viscous supersonic laminar flow and the Shock Wave- Laminar Boundary Layer Interaction (SWBLI) around the F-16 laminar NACA 6-series airfoil NACA 64A204. The study aims t

Externí odkaz: http://arxiv.org/abs/2301.01135

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Improved Analytical/Statistical Modelling of the Shock Wave-Laminar Boundary Layer Around a Thin Airfoil Standard Atmosphere Case

Autor: Eddegdag, N., El-Aajine, O., Naamane, A., Radouani, M.

The aim of this present work is to develop an improved and more precise analytical modelling of a steady irrotational laminar Shock Wave- Boundary Layer Interaction for weak shockwaves around a thin airfoil at a low incidence in the standard atmosphe

Externí odkaz: http://arxiv.org/abs/2212.11321

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