Numerical Study of Central Secondary Injection in a   Planar, Profiled Divergent Nozzle

dc.contributor.author	BENSAAD, Rabah Abdelbasset;
dc.contributor.author	LARIBI, Meriem ;
dc.contributor.author	Mr. KBAB, Hakim(promoteur);
dc.date.accessioned	2025-09-28T09:44:31Z
dc.date.available	2025-09-28T09:44:31Z
dc.date.issued	2025
dc.identifier.uri	https://di.univ-blida.dz/jspui/handle/123456789/40501
dc.description	019/2025 option: Propulsion	fr_FR
dc.description.abstract	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 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 waves	fr_FR
dc.language.iso	en	fr_FR
dc.publisher	blida01	fr_FR
dc.title	Numerical Study of Central Secondary Injection in a Planar, Profiled Divergent Nozzle	fr_FR
dc.type	Thesis	fr_FR