Compréhension du comportement vibro-acoustique du plancher de la zone non simulée des simulateurs de vol : déterminer les facteurs plus influents.

Les simulateurs de vols sont devenus des instruments indispensables pour former les pilotes et membres d’équipages. Le leader mondial dans la conception de ces simulateurs est CAE, une entreprise Canadienne comptant plus de 10 000 salariées. Cependant, afin de garder une longueur d’avance sur ses concurrents, il lui est nécessaire de constamment les performances de […]

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LR-FHSS-base network size estimation for dts-iot

The project’s goal is to find out if the network size estimator L-OCI, designed for direct-to satellite Internet of Things LoRa based scenarios, can be extended and/or adapted to work based on LR-FHSS. We want to see if they can handle many devices, and whether this combination is good or bad for a specific problem. […]

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Design and Life Cycle Analysis of Electric Aircraft Propulsion Systems

In collaboration with CAE, the project’s primary goal is to identify an appropriate material to isolate a battery pack in a hybrid electric aircraft. The chosen material must be as light as possible, while meeting appropriate safety standards. This battery module will be integrated into an aircraft for testing by the industry partner. With a […]

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An Intelligent Method for Bearing Anomaly Detection

Anomaly detection of machinery is a crucial aspect of predictive maintenance. It involves monitoring specific parameters related to the machinery’s condition to identify significant changes that indicate a potential fault. Bearings, which are important components in rotary machinery, are responsible for over 40 percent of rotary machinery failures. Consequently, researchers have been focusing on detecting […]

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AI-powered Solutions for Complex Systems

AI tools based on deep learning has recently been suggested for many complex problems where a large amount of data is available. We will be working similar AI tools but problems from very different domains, namely, airport delay management after disruption and predicting prices of fresh produce under challenging climate conditions. Establishing a recovery flight […]

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Measuring the dark matter halo mass distribution with weak gravitational lensing using the Ultraviolet Near-Infrared Optical Northern Survey

In this project, the results from Ultraviolet Near-Infrared Optical Northern Survey will be used to model dark matter mass distribution around galaxies in the galactic cluster. Observing weak gravitational lensing of background galaxies from the optical multi-band survey and determining its parameters will help us to simulate dark matter halos around galaxies, that cause lensing, […]

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Vortex Identification Using Machine Learning

Many fluid flows are dominated by the dynamics of vortex formation and convection. Examples of practical importance include flows over aircraft wings/wind turbine blades and environmental flows. Knowledge of vortex parameters such as position, radius, circulation, and convective velocity are needed to understand and predict the influence of vortices on flow development. Although a vortex […]

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Development of purification for high-quality boron nitride nanotube liquid crystals

Boron nitride nanotube (BNNT), a structural analog of carbon nanotube, has emerged as a key-enabling material in various fields of extreme/major science thanks to its transformative properties such as high oxidation resistance, high specific mechanical strength, piezoelectricity, and high neutron shielding capability. To harness its unique properties, it is essential to fabricate macroscopic BNNT articles […]

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Avion sans pilote dans l’atmosphère martienne

Objectif: Conception préliminaire par analyse seulement d’un avion capable d’effectuer un vol propulsé et autonome dans l’atmosphère de Mars. Travail individuel sous supervision. – Préparation: conception d’un avion, atmosphère martienne, revue de la littérature scientifique – Liste des requis, mission typique, préparation du cahier des charges – Estimation du poids initial – Performance aérodynamique: charge […]

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Performance d’un fuselage intégré hybride en régime transsonique

En 2015, la NASA, Boeing et Pratt & Whitney ont entrepris des études expérimentales et numériques pour calculer les performances d’un fuselage intégré hybride (HWB), désigné N2A-EXTE 0009H1, pour tous les régimes de vol, dont celles en transsonique. Le but de ces études était de vérifier un concept d’intégration moteur avec cette cellule d’avion non-conventionnelle. […]

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