Numerical Analysis of Pulse Decay Characteristics in Solid Rocket Motors for Different Finocyl Grain Configurations

Combustion instability is an abnormal working state that often occurs in advanced solid rocket motors (SRMs), which can arouse pressure oscillations, increase the risk of mission failure, and even cause structural damage. In this paper, a numerical simulation method is adapted to analyze the combust...

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Bibliographic Details
Main Authors: Fengnan Guo, Fengrui Li, Hongfeng Ji, Lin Fu, Xuyang Gao
Format: Article
Language:English
Published: MDPI AG 2025-06-01
Series:Aerospace
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Online Access:https://www.mdpi.com/2226-4310/12/6/537
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