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The document describes a numerical study of a two-fluid model to analyze thrust and pressure perturbations in solid rocket motors during the ejection of inert particles. It outlines the development of a numerical model to solve the governing Euler equations in two stages - first without a particle to obtain nominal values, then introducing a particle and modeling its drag force. Four cases are analyzed with particles of different sizes released at different locations. The results show the single-phase simul
- Author
- VenuAgarwal
- Language
- EN