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 (...

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Bibliografski detalji

Glavni autori:	Nabila ALILI, Khacem KADDOURI, Salem MOKADEM, Ahmed ALAMI
Format:	Artigo
Jezik:	Inglês
Izdano:	National Institute for Aerospace Research “Elie Carafoli” - INCAS 2024-03-01
Serija:	INCAS Bulletin
Teme:	rocket engine nozzle k-epsilon turbulence model convergence angle divergence angle gross thrust coefficient velocity coefficient
Online pristup:	https://bulletin.incas.ro/files/alili_kaddouri_mokadem_alami__vol_16_iss_1.pdf
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