|国家科技期刊平台
首页|期刊导航|南京航空航天大学学报|高超声速带奇性轴外形热流准确预示的混合算法研究与应用

高超声速带奇性轴外形热流准确预示的混合算法研究与应用OA北大核心CSTPCD

Research on Hybrid Algorithm for Accurate Heat Flux Prediction on Hypersonic Flows with Singularity Axis

中文摘要英文摘要

准确的热流预示在超/高超声速复杂流动数值模拟是一个难点问题.当计算网格中出现奇性轴时,进一步增加了准确流场模拟、热流计算的难度.本文针对奇性轴在有限差分计算中出现的流场结构不稳定、热流预测误差大等难题,在通量重构方法的基础上,结合基于守恒变量的重构方法,提出了一种采用高精度格式计算带奇性轴问题的混合算法.该算法在奇性轴附近使用基于守恒变量的重构方法,有效反映奇性轴附近流场分布对奇性轴计算的影响,能够有效解决奇性轴问题.采用该混合算法并对比应用 WENO3-JS 和高分辨率WENO3-PRM21,1 格式,本文对高超声速球头、HB-2、球钝锥及Apollo等外形绕流问题进行了数值模拟,结果表明:新方法能够有效解决含奇性轴问题计算中的流场结构不稳定问题,并且可以实现准确的热流预示.

Accurate heat flux prediction is a key problem in the numerical simulation of hypersonic flows.When the singularity axis appears in the grid,it further increases the difficulty of accurate flow simulation and heat flux calculation.Aiming at the problems of instability of flow structure and large errors of heat flux prediction in the finite difference calculation of singularity axis problems,a hybrid algorithm for solving the singularity axis problem with high-precision difference schemes is proposed by combining the flux reconstruction and conservation reconstruction.The algorithm is based on conservative variables reconstruction near the singularity axis,which can reflect the influence of the flow field distribution near the singularity axis.The algorithm can effectively solve the singularity axis problem in numerical simulation.Applying the hybrid algorithm with WENO3-JS and WENO3-PRM21,1 scheme,the numerical simulations of hypersonic flow around sphere,HB-2,sphere cone and Apollo are carried out.The results show that the new method can effectively solve the problems of flow instability with singularity axis,and can achieve accurate heat flux prediction.

谭国灼;李沁;黄潇;翁谊辉;严攀;尤延铖

厦门大学航空航天学院,厦门 361102

高超声速气动热奇性轴混合算法高精度格式

hypersonicaerodynamic heatsingularity axishybrid algorithmhigh accuracy scheme

《南京航空航天大学学报》 2024 (004)

609-621 / 13

10.16356/j.1005-2615.2024.04.003

评论