研究论文

不同飞行高度下超声速来流/射流及其相互作用的数值模拟

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  • 1.上海大学 上海市应用数学和力学研究所, 上海 200072
    2.中国科学院力学研究所 高温气体动力学国家重点实验室, 北京 100190
    3.中国科学院大学 工程科学学院, 北京 100049
韩桂来(1984—), 男, 副研究员, 研究方向为高超声速边界层及转捩现象. E-mail:hanguilai@imech.ac.cn

收稿日期: 2019-01-11

  网络出版日期: 2019-05-30

基金资助

国家自然科学基金资助项目(11472281,);国家自然科学基金资助项目(11532014);国家重点研发计划资助项目(2016YFA0401200)

Numerical simulation of the supersonic flow/jet flow and their interaction at different flight altitudes

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  • 1. Shanghai Institute of Applied Mathematics and Mechanics, Shanghai University, Shanghai 200072, China
    2. State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
    3. School of Engineering Science, University of Chinese Academy of Sciences, Beijing 100049, China

Received date: 2019-01-11

  Online published: 2019-05-30

摘要

采用高精度格式求解二维Navier-Stokes方程, 研究了不同飞行高度下超声速来流和射流在后台阶相互作用的流场基本结构. 时间推进采用三阶精度Runge-Kutta格式, 分别应用五阶精度加权本质无振荡(weighted essentially non-oscillatory, WENO)格式、六阶精度中心差分格式来离散对流项和粘性项, 并应用MPI非阻塞式实现并行化. 采用两步后台阶模型分别研究了不同高度下超声速后台阶流动、 射流的基本结构特征; 并进一步组合两种流动, 研究了超声速来流/射流组合流动下相互作用的流场结构. 通过改变后台阶上方来流条件, 模拟了不同飞行高度的环境, 研究了其对流场中涡、剪切层、激波等结构的影响. 研究结果发现, 超声速来流和射流发生相互作用后, 在后台阶附近产生回流区, 超声速来流的存在会对射流的流场结构产生影响.

本文引用格式

邓放, 韩桂来, 刘美宽, 丁珏, 翁培奋, 姜宗林 . 不同飞行高度下超声速来流/射流及其相互作用的数值模拟[J]. 上海大学学报(自然科学版), 2021 , 27(2) : 307 -324 . DOI: 10.12066/j.issn.1007-2861.2147

Abstract

The two-dimensional Navier-Stokes equations were solved using high-precision schemes, and the basic structure of the flow field in the supersonic flow and jet flow at different flight altitudes was studied. The three-order Runge-Kutta scheme was adopted in the time-marching scheme. The five-order weighted essentially non-oscillatory (WENO) and the six-order central difference schemes were used to discretize the convection term and viscous term, respectively. The parallel computation was performed using MPI non-blocking communication. The basic structural characteristics of backward-facing step flow and jet flow under backward-facing steps at different flight altitudes were studied. Furthermore, by combining the two flows, the flow field structure of the interaction between the supersonic flow and jet flow was studied. The supersonic flow above the backward-facing step was changed to simulate the environment of different flight altitudes, and the environment affected structures such as vortices, shear layers, and shock waves in the flow field. It was observed that after the interaction between the supersonic flow and jet flow, a recirculation zone was generated near the back step, and the presence of supersonic flow affected the structures of the jet flow.

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