Numerical Analysis of Convergent-Divergent Angles and Operating Conditions Impact on Rocket Nozzle Performance Parameters

Comprehensive numerical analysis was conducted to elucidate the exhaust performance of rocket engine nozzles. The study focused on unravelling the intricate relationship between convergence and divergence angles and their impact on the exhaust performance parameters, including velocity coefficient (...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής

Κύριοι συγγραφείς:	Nabila ALILI, Khacem KADDOURI, Salem MOKADEM, Ahmed ALAMI
Μορφή:	Artigo
Γλώσσα:	Inglês
Έκδοση:	National Institute for Aerospace Research “Elie Carafoli” - INCAS 2024-03-01
Σειρά:	INCAS Bulletin
Θέματα:	rocket engine nozzle k-epsilon turbulence model convergence angle divergence angle gross thrust coefficient velocity coefficient
Διαθέσιμο Online:	https://bulletin.incas.ro/files/alili_kaddouri_mokadem_alami__vol_16_iss_1.pdf
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