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固体推进剂加工工艺的光滑粒子动力学数值仿真

王智泓 王春光 王悦聪 刘一新 李易寒

固体火箭技术2026,Vol.49Issue(2):290-303,14.
固体火箭技术2026,Vol.49Issue(2):290-303,14.DOI:10.7673/j.issn.1006-2793.2026.02.014

固体推进剂加工工艺的光滑粒子动力学数值仿真

Numerical simulation of solid propellant processing technology based on smoothed particle hydrodynamics

王智泓 1王春光 2王悦聪 1刘一新 1李易寒1

作者信息

  • 1. 西安交通大学 航天航空学院,复杂服役环境重大装备结构强度与寿命全国重点实验室,西安 710049
  • 2. 西安交通大学 航天航空学院,复杂服役环境重大装备结构强度与寿命全国重点实验室,西安 710049||北京凌空天行科技有限责任公司,北京 100176
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摘要

Abstract

During solid propellant production,multi-component particles and binders need to be stirred in a mixing kettle to form a slurry and then pressure-poured into the motor chamber.The complex interfacial dynamics of multiphase components during mixing,along with the high yield stress and the discontinuous extrusion of slurry during casting are difficult to be effectively simulated by means of traditional grid-based methods.Based on the smoothed particle hydro-dynamics(SPH)method,combined with the Herschel-Bulkley-Papanastasiou constitutive model and the multi-component description framework,a numerical model suitable for the mixing and casting processes of solid propellant slurry was established,and the mixing experiment was carried out.The results show that this method has high accuracy while simulating Newtonian and non-Newtonian fluids.The simulation deviations of Np-Re power characteristic curves of Newtonian and non-Newtonian fluids are 7.6%and 1.7%,respectively.SPH simulations of planetary mixing reveal chaotic effect from stirring and kneading of solid and hollow double blades,as well as the synergistic effect of high-vorticity hot spots.After mixing,the slurry reaches a uniform state with a density difference within≤80 kg/m3,and the uniformity square deviation tends to be stabilize after four evolutionary stages.The shear-thinning of the mixture promotes the formation of spiral band of high-vorticity hot spots near hollow blades.For vacuum casting,the SPH simulation completely captures the extrusion-fracture-retraction,leveling accumulation and wetting penetration behavior of the slurry,and verifies dislocation arrangement effectiveness of the core mold and the pouring hole,indicating that the liquid level is highly consistent in the area away from the injection hole,and the slurry has good leveling.

关键词

固体推进剂/SPH方法/非牛顿流体/行星式混合/真空浇注

Key words

solid propellant/smoothed particle hydrodynamics/Non-Newtonian fluid/planetary mixting/vacuum casting

分类

航空航天

引用本文复制引用

王智泓,王春光,王悦聪,刘一新,李易寒..固体推进剂加工工艺的光滑粒子动力学数值仿真[J].固体火箭技术,2026,49(2):290-303,14.

基金项目

全国重点实验室开放基金(NKLACP220241B13). (NKLACP220241B13)

固体火箭技术

1006-2793

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