水下固体发动机尾流场数值仿真

推进技术 ›› 2009, Vol. 30 ›› Issue (4): 479-483.

水下固体发动机尾流场数值仿真

向敏,吴雄,张为华,王中伟

国防科技大学航天与材料工程学院;国防科技大学航天与材料工程学院;国防科技大学航天与材料工程学院;国防科技大学航天与材料工程学院

发布日期:2021-08-15

Numerical simulation for underwater solid motor tail flow

Inst.of Aerospace and Material Engineering,National Univ.of Defence Technology,Changsha 410073,China;Inst.of Aerospace and Material Engineering,National Univ.of Defence Technology,Changsha 410073,China;Inst.of Aerospace and Material Engineering,National Univ.of Defence Technology,Changsha 410073,China;Inst.of Aerospace and Material Engineering,National Univ.of Defence Technology,Changsha 410073,China

Published:2021-08-15

摘要/Abstract

摘要： 基于轴对称非定常可压缩N-S方程和VOF两相流模型,对水下固体发动机尾流场进行了数值仿真。结果较好地预示了尾流场燃气泡生长过程,得到了水下发动机工作初期尾流场形态及其演化过程。对发动机在水下和地面两种工况下的性能进行了对比。

关键词: 固体推进剂火箭发动机;水下火箭;尾流;二相流;流场仿真

Abstract: Based on axisymmetric unsteady-compressible N-S equations and VOF multiphase model,underwater solid motor tail flow was numerically simulated.Results show that well it has been well predicted for the growth process of the gas bubble in tail flow,as well as the shape and evolution process for tail flow.Then,work performance has been compared between motor working on the ground and working underwater.

Key words: Solid propellant rocket engine;Underwater rocket;Wake;Two phase flow;Flow field simulation

向敏,吴雄,张为华,王中伟. 水下固体发动机尾流场数值仿真[J]. 推进技术, 2009, 30(4): 479-483.