Please use this identifier to cite or link to this item: http://localhost:8080/xmlui/handle/123456789/40501
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dc.contributor.authorBENSAAD, Rabah Abdelbasset;-
dc.contributor.authorLARIBI, Meriem ;-
dc.contributor.authorMr. KBAB, Hakim(promoteur);-
dc.date.accessioned2025-09-28T09:44:31Z-
dc.date.available2025-09-28T09:44:31Z-
dc.date.issued2025-
dc.identifier.urihttps://di.univ-blida.dz/jspui/handle/123456789/40501-
dc.description019/2025 option: Propulsionfr_FR
dc.description.abstractThe 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 divergent nozzle. The main objective is to evaluate the influence of this injection on the supersonic flow, by examining changes in jet structure, pressure distribution, and the possible alterations in internal shock wavesfr_FR
dc.language.isoenfr_FR
dc.publisherblida01fr_FR
dc.titleNumerical Study of Central Secondary Injection in a Planar, Profiled Divergent Nozzlefr_FR
dc.typeThesisfr_FR
Appears in Collections:Mémoires de Master

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