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...

Celý popis

Podrobná bibliografie

Hlavní autoři:	Dongjian Su, Qingyu Lin, Hao Wang, Ruyi Tao
Médium:	Artigo
Jazyk:	Inglês
Vydáno:	MDPI AG 2024-07-01
Edice:	Aerospace
Témata:	solid rocket motor immersed boundary method face offsetting method burning surface regression erosive burning
On-line přístup:	https://www.mdpi.com/2226-4310/11/7/550
Tagy:	Přidat tag Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!