固相颗粒在C1xb固体火箭发动机中的运动规律

Translated title of the contribution: Motion Trajectory of Solid Particles in C1xb Solid Rocket Motor

Xingpeng Gu, Junwei Li*, Wensheng Qiao, Sheng Wu, Lei Han, Qi Wang, Ningfei Wang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

The force of condensed-phase particles in C1xb solid rocket motor (SRM) is analyzed based on internal flow field of motor. The velocity and acceleration of particle at different moments are obtained, and a two-dimensional particle motion trajectory model is established. Based on this model, the spatial distribution rule of particles in SRM is obtained. On this basis, the effects of motor rotation, initial position of particle and particle size on the movement of condensed-phase particles are studied. Results show that the particles leaving the upstream and downstream surfaces of aluminized hydroxyl-terminated-polybutadiene propellant have a greater probability of colliding with inner wall. Larger size particles increase the probability of collision with inner wall during particle movement. Rotation has more influence on spatial distribution of particles in motor in comparison with axial overload.

Translated title of the contributionMotion Trajectory of Solid Particles in C1xb Solid Rocket Motor
Original languageChinese (Traditional)
Pages (from-to)489-502
Number of pages14
JournalBinggong Xuebao/Acta Armamentarii
Volume43
Issue number3
DOIs
Publication statusPublished - Mar 2022

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