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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
Appears in Collections:Mémoires de Master

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