Numerical Simulation of Gas Flow Coupled with Burning Surface Regression Based on Immersed Boundary Method and Face Offsetting Method

The coupling action of gas flow with propellant burning surface regression is the critical process in solid rocket motor (SRM), which has an important effect on the unsteady combustion, erosive burning, dynamic combustion and pressure fluctuation of propellants. The immersed boundary method (IBM) is...

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Bibliographic Details

Published in:	Aerospace
Main Authors:	Dongjian Su, Qingyu Lin, Hao Wang, Ruyi Tao
Format:	Article
Language:	English
Published:	MDPI AG 2024-07-01
Subjects:	solid rocket motor immersed boundary method face offsetting method burning surface regression erosive burning
Online Access:	https://www.mdpi.com/2226-4310/11/7/550