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2023 | OriginalPaper | Buchkapitel

Numerical Simulation of Reacting Flow Field in a Solid-Propellant Ducted Rocket

verfasst von : Nitin Sharma, Yash Pal, Vivek Warade

Erschienen in: Energy and Exergy for Sustainable and Clean Environment, Volume 2

Verlag: Springer Nature Singapore

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Abstract

The scope of the current study is to estimate the flow fields in reacting and non-reacting flow regimes of a solid-propellant ducted rocket combustor (SDRC) at different ram duct angles. The 2D simulation and combustion modelling of the reacting and non-reacting flow were carried out using OpenFOAM. The flow fields and the mass fraction distribution were computationally modelled and qualitatively compared. The predicted axial and vertical flow velocities were compared with the experimental and analytical results from the literature to validate the current study at different ram duct angles. The performance in terms of flow velocity and mass fraction was found out to be the highest in the 45° configuration.

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Metadaten
Titel
Numerical Simulation of Reacting Flow Field in a Solid-Propellant Ducted Rocket
verfasst von
Nitin Sharma
Yash Pal
Vivek Warade
Copyright-Jahr
2023
Verlag
Springer Nature Singapore
DOI
https://doi.org/10.1007/978-981-16-8274-2_18