This study focuses on the development of a flight controller for drones, utilizing both
classic PIC microcontrollers and dsPICs to optimize performance. The main objective
is to design and implement an embedded system ...
BENSAAD, Rabah Abdelbasset;; LARIBI, Meriem ;; Mr. KBAB, Hakim(promoteur);(blida01, 2025)
The optimization of flow within nozzles plays a key role in enhancing the performance of
aerospace propulsion systems. This numerical study focuses on analyzing the effect of central
secondary injection in a planar ...
TAMADARTAZA, Amayes;; LOUAZANI, Mustapha Younes;; Dr. ALLOUCHE, Rachid (promoteur);; Dr. RENANE, Rachid (promoteur);(blida01, 2025)
Ce mémoire traite de la conception et de l’optimisation aérodynamique d’une éolienne
à axe horizontal adaptée aux conditions venteuses en Algérie. Une approche multiétape
a été adoptée, comprenant une modélisation ...
In this study, two types of rocket fuel tanks were analyzed: a cylindrical tank, a spherical tank
and a wing profile containing an integrated tank.
Modal analysis was performed using ANSYS and COMSOL to evaluate the ...
Ce mémoire présente une étude expérimentale et numérique de l’écoulement de l’air
autour d’un profil d’aile symétrique NACA 0012 en régime subsonique.
L’objectif principal est d’évaluer la distribution du coefficient ...
Course Objectives: This course is designed for Master's level students specializing in avionics. It aims to equip students with comprehensive knowledge and practical skills in managing complex projects within the aeronautical ...
Aerospace researchers and engineers seek to develop and improve this field in various branches to become safer and lighter at the lowest cost, including turbines, where it has been striving to improve its performance, in ...
Résumé: Ce cours s'adresse aux étudiants L3 option structures avions, il présente de manière générale l'évolution des matériaux composites dans le domaine aéronautique et aérospatiale, leurs propriétés thermoélastique et ...
Objectifs du Cours: Ce cours s'adresse aux étudiants Master II option structures aéronautiques, Les étudiants auront une vue complète sur la notion d'un projet et comprendront comment faire la planification, l'ordonnancement, ...
In aviation, flight controls are the systems that connect the pilot to the aerodynamic control surfaces, allowing for changes in the aircraft's attitude and trajectory. These systems consist of control devices (such as the ...
The work developed in this thesis focuses on the implementation of control techniques, such as PID and fuzzy PID, to assess their performance in both longitudinal and lateral modes for a fixed-wing drone. We expand on how ...
This thesisprojectinvestigates combustion in a semi-industrialchamberfueled by naturalgas and oxygen, utilizingnumerical simulations conductedwith ANSYS-Fluent. The mathematical model isbased on solving the Navier-Stokes ...
Generally, the internal flow in turbomachines is characterized by its viscosity, its compressibility, its three-dimensionality and its vortices. As part of various research on centrifugal compressors, many researchers have ...
Bahi, Abd el adim; Amziane, Khalil; Laazab, Sebaa (promoteur); Bekhti, Ahmed (promoteur)(Université Blida 01, 2024)
The use of computational fluid dynamics (CFD) has become essential in the design of centrifugal compressors, offering the ability to predict key performance metrics such as pressure ratio and efficiency with a reasonable ...
Khediri, Dounia Zed; Chegrani, Ahmed (promoteur)(Université Blida 01, 2024)
This thesis presents a theoretical and numerical study of the longitudinal and lateral- directional stability of an aircraft. This work aims to determine the characteristics of an aircraft's stability and its response to ...
Kaddouri, Hind Yasmine; Krim, Mohamed (promoteur); Mehaya, Mohammed Mehdi (promoteur)(Université Blida 01, 2024)
This study presents the design, development, and evaluation of an inertially stabilized airborne camera control system utilizing a 3-axis gimbal for UAV-based active object tracking.
The proposed system is designed to ...
Saoudi, Sara; Chegrani, Ahmed (promoteur)(Université Blida 01, 2024)
This projet deals with the static stability of an aircraft and a drone in the subsonic regime. The first part consists of a study of the concepts of static stability in the longitudinal and lateral- directional cases. In ...
Centrifugal compressors rarely perform exactly as designed due to uncertainties in manufacturing and operation. These uncertainties can negatively impact The actual compressor performance, leading to instability. However, ...