Agglomerate Size Evolution in Solid Propellant Combustion under High Pressure

Agglomerate Size Evolution in Solid Propellant Combustion under High Pressure

Solid propellant combustion and flow are significantly affected by condensed combustion products (CCPs) in solid rocket motors. A new aluminum agglomeration model is established using the discrete element method, considering the burning rate and formulation of the propellant. Combining the aluminum...

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Bibliographic Details
Main Authors: Songchen Yue, Lu Liu, Huan Liu, Yanfeng Jiang, Peijin Liu, Aimin Pang, Guangxue Zhang, Wen Ao
Format: Article
Language:English
Published: MDPI AG 2023-05-01
Series:Aerospace
Subjects:
aluminized solid propellant
condensed combustion products
agglomeration
combustion
particle size prediction model
Online Access:https://www.mdpi.com/2226-4310/10/6/515

Internet

https://www.mdpi.com/2226-4310/10/6/515

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