Veuillez utiliser cette adresse pour citer ce document : https://di.univ-blida.dz/jspui/handle/123456789/40474
Affichage complet
Élément Dublin CoreValeurLangue
dc.contributor.authorMellouk, Islem Hafedh;-
dc.contributor.authorAbada, Omar(promoteur);-
dc.contributor.authorAbdallah Elhirtsi, AHMED( Promoteur);-
dc.date.accessioned2025-09-24T12:27:45Z-
dc.date.available2025-09-24T12:27:45Z-
dc.date.issued2025-
dc.identifier.urihttps://di.univ-blida.dz/jspui/handle/123456789/40474-
dc.description006/2025 option: structurefr_FR
dc.description.abstractIn 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 impact of various parameters (shape, material, thickness, etc.) on the natural frequencies. The results showed that some factors have a significant influence on the frequencies, while others have a limited effect. A good agreement was observed between the results from both software tools.fr_FR
dc.language.isofrfr_FR
dc.publisherblida01fr_FR
dc.subjectModal analysis;fr_FR
dc.subjectVibration;fr_FR
dc.subjectFinite element method;fr_FR
dc.subjectRocket;fr_FR
dc.titleAnalyse modale et étude des fréquences propres des réservoirs de carburant pour moteur-fuséefr_FR
dc.typeThesisfr_FR
Collection(s) :Mémoires de Master

Fichier(s) constituant ce document :
Fichier Description TailleFormat 
Thése Mellouk Version final corrigé.pdf5,4 MBAdobe PDFVoir/Ouvrir


Tous les documents dans DSpace sont protégés par copyright, avec tous droits réservés.