Contribution to the Study of the Numerical Simulation of Compressible Flow in a Convergent-divergent Nozzle
A. Ederouich, M. Essahraoui, D. Zejli, A. Saad
2021
Abstract
The use of a convergent-divergent nozzle meets several needs, namely the study of the performance of wind turbines, turbine engine blades, aeroplane wings, and propellants. In this work, we have been studying compressible flow of an ideal gas in a one-dimensional convergent-divergent nozzle essentially. The study aims at determining the evolution of all the parameters of the flow along with the Nozzle (the pressure, temperature, Mach number, and density). Thus, we studied the influence of the nozzle geometry on the flow by the variation of the diverging angle. The numerical simulation of the flow has been carried out using the ANSYS Fluent software, which uses the finite volume method to solve the various partial differential equations modelling the physical phenomenon. The results obtained from this model have been compared with the theoretically calculated results. Good agreement was observed.
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in Harvard Style
Ederouich A., Essahraoui M., Zejli D. and Saad A. (2021). Contribution to the Study of the Numerical Simulation of Compressible Flow in a Convergent-divergent Nozzle. In Proceedings of the 2nd International Conference on Big Data, Modelling and Machine Learning - Volume 1: BML, ISBN 978-989-758-559-3, pages 360-365. DOI: 10.5220/0010734400003101
in Bibtex Style
@conference{bml21,
author={A. Ederouich and M. Essahraoui and D. Zejli and A. Saad},
title={Contribution to the Study of the Numerical Simulation of Compressible Flow in a Convergent-divergent Nozzle},
booktitle={Proceedings of the 2nd International Conference on Big Data, Modelling and Machine Learning - Volume 1: BML,},
year={2021},
pages={360-365},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0010734400003101},
isbn={978-989-758-559-3},
}
in EndNote Style
TY - CONF
JO - Proceedings of the 2nd International Conference on Big Data, Modelling and Machine Learning - Volume 1: BML,
TI - Contribution to the Study of the Numerical Simulation of Compressible Flow in a Convergent-divergent Nozzle
SN - 978-989-758-559-3
AU - Ederouich A.
AU - Essahraoui M.
AU - Zejli D.
AU - Saad A.
PY - 2021
SP - 360
EP - 365
DO - 10.5220/0010734400003101