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

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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Bibliographic Details
Main Authors: Nabila ALILI, Khacem KADDOURI, Salem MOKADEM, Ahmed ALAMI
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2024-03-01
Series:INCAS Bulletin
Subjects:
rocket engine nozzle
k-epsilon turbulence model
convergence angle
divergence angle
gross thrust coefficient
velocity coefficient
Online Access:https://bulletin.incas.ro/files/alili_kaddouri_mokadem_alami__vol_16_iss_1.pdf

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