Numerical simulation of particle erosion in the internal flow field of solid rocket motor nozzle using Rocstar
Solid composite propellants often contain metal particles, such as aluminum particles, and the internal flow field in a solid rocket motor is a typical gas–solid two-phase flow field. In this study, to address the problem of the erosion of particles on the wall during the working process of an engin...
Main Authors: | Wei Zhou, Yongqi Yin, Zhensheng Sun, Peiyang Ma, Xueqian Shi |
---|---|
Format: | Article |
Language: | English |
Published: |
AIP Publishing LLC
2022-12-01
|
Series: | AIP Advances |
Online Access: | http://dx.doi.org/10.1063/5.0113612 |
Similar Items
-
The Submerged Nozzle Damping Characteristics in Solid Rocket Motor
by: Xiaosi Li, et al.
Published: (2023-02-01) -
Study on the Influence of Nozzle Ablation on the Performance of the Solid Rocket Motor
by: Weiqiang Huang, et al.
Published: (2023-02-01) -
Investigation of solid propellant rocket motor nozzle via CFD simulation
by: Aolin, Chen, et al.
Published: (2020) -
Transient Characteristics of Fluidic Pintle Nozzle in a Solid Rocket Motor
by: Dongfeng Yan, et al.
Published: (2024-03-01) -
Study on Separation Characteristics of Nozzles with Large Expansion Ratio of Solid Rocket Motors
by: Zhihong Wang, et al.
Published: (2022-12-01)