摘要
Two-phase flow in the solid rocket motor combustion chamber under overload condition is studied with numerical method. A 2-D plane particle-trajectory model is developed, and second order upwind scheme is applied to construct the finite volume calculation modular. With this algorithm, several flow regimes with or without overload are calculated and some effects of overload on the particle trajectories and gas phase are established. The simulation results are useful to the research of operation procedure and thermal structure design of the motor.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 8-12 |
| 页数 | 5 |
| 期刊 | Guti Huojian Jishu/Journal of Solid Rocket Technology |
| 卷 | 24 |
| 期 | 2 |
| 出版状态 | 已出版 - 2001 |