高速气固两相横向射流数值模拟进展

马立坤; 徐路淅; 杨鹏年; 夏智勋; 冯运超

doi:10.13224/j.cnki.jasp.20240512

高速气固两相横向射流数值模拟进展

doi: 10.13224/j.cnki.jasp.20240512

国防科技大学高超声速技术实验室，长沙 410073

基金项目: 国家自然科学基金（12272409，U21B2086）

详细信息

作者简介:
马立坤（1987-），男，副教授，博士，研究方向为高超声速推进技术。E-mail：malikun@nudt.edu.cn

通讯作者:
徐路淅（2000-），男，博士生，研究方向为高超声速推进技术。E-mail：xuluxi18@nudt.edu.cn

中图分类号: V435
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出版历程
- 收稿日期: 2024-07-28
- 网络出版日期: 2024-12-04

Progress in numerical simulation of gas-solid two-phase jet in high-speed crossflow

Hypersonic Technology Laboratory，National University of Defense Technology，Changsha 410073，China

摘要

摘要:
从数值模拟方法、颗粒弥散特性和颗粒对流动的作用3个方面进行概述，回顾了近些年来国内外对高速气固两相横向射流数值模拟研究的进展。欧拉-拉格朗日方法是高速气固稀疏两相流研究的一般模拟方法，颗粒的分布受射流流动结构和颗粒自身性质影响，颗粒在射流流场中的优先聚集与气流密度和涡量相关，大颗粒的引入会改变射流的流动结构，且会削弱湍流强度。认为可进一步改进射流出口边界条件和数值方法以提高模拟的准确性；补充复杂构型和多工况的高精度数据，基于机器学习方法建立快速预测模型。
- 固体火箭超燃冲压发动机 /
- 气固两相流 /
- 横向射流 /
- 高速气流 /
- 两相数值模拟
Abstract:
The progresses in numerical simulation methods, particle dispersion characteristics, and particle effects on flows for high-speed gas-solid two-phase transverse jets in recent years were reviewed. Result showed that, the Eulerian-Lagrangian method is a general simulation approach for studying high-speed gas-solid sparse two-phase flows. The distribution of particles was influenced by the jet flow structure and particle properties, the preferential concentration of particles in the jet flow field was related to the airflow density and vorticity, large particles can change the flow structure of the jet and weaken the turbulence intensity. It was believed that the boundary conditions and numerical methods for the jet outlet could be further improved to enhance the accuracy of the simulation; high-precision data for complex structures and multiple conditions should be supplied to establish a fast prediction model based on machine learning methods.
- solid rocket scramjet /
- gas-solid two-phase flow /
- transverse jet /
- high-speed flow /
- two-phase numerical simulation

HTML

图 1 超声速横向射流时间平均结构示意图^[13]

Figure 1. Average time structure of transverse jet in supersonic flow^[13]

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图 2 不同时间、空间尺度与体积分数适用的两相流动模拟方法^[30]

Figure 2. Two phase flow simulation methods applicable to different time, spatial scales and volume fractions^[30]

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图 3 对称平面的流场速度云图和按速度着色的粒子在面上的投影^[53]

Figure 3. Contours of velocity in symmetry plane for the supersonic jet and particles colored by velocity was project in the plane^[53]

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图 4 流向平面x/D=35处瞬时密度和流向涡量云图与大颗粒分布情况^[55]

Figure 4. Instantaneous density and flow vorticity cloud map and distribution of large particles at x/D=35 on flow plane^[55]

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图 5 流向平面x/D=35处瞬时密度和流向涡量云图与小颗粒分布情况^[55]

Figure 5. Instantaneous density and flow vorticity cloud map and distribution of small particles at x/D=35 on flow plane^[55]

下载: 全尺寸图片幻灯片

图 6 展向区间−0.5≤z/D≤0.5内平均边界层厚度$\delta $沿流向发展^[55]

Figure 6. Average boundary layer thickness within the spanwise interval of −0.5≤z/D≤0.5 develops along flow direction^[55]

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图 7 不同粒径颗粒沿轴向截面的湍流强度^[56]

Figure 7. Turbulence intensity of particles with different particle sizes along axial cross-sections^[56]

下载: 全尺寸图片幻灯片

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