Numerical Investigation on the Mechanism of Solid Rocket Motor Instability Induced by Differences between On-Ground and In-Flight Conditions

A solid rocket motor (SRM) with a high aspect ratio that performs normally during ground tests may experience instability during flight. To address this issue, this study employs the pulse triggering method and the numerical approach of two-way fluid–structure interaction to investigate the mechanis...

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Bibliographic Details
Main Authors: Ge Wang, Chengke Li, Weiqiang Pu, Bocheng Zhou, Haiwei Yang, Zenan Yang
Format: Article
Language:English
Published: MDPI AG 2024-03-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/11/3/215