hzf@tju.edu.cn
流体力学
无
副教授
机翼边界层的稳定性分析和转捩预测研究

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超音速钝平板边界层感受性系数的研究

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某海域波浪演化的数值仿真

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火灾模拟程序并行计算运行

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复杂地形海域三维波浪计算源代码开发

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流体流动数值仿真技术

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应用技术

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后掠机翼流动机理的研究

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小攻角后掠翼边界层的稳定性分析和转捩预测

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超音速湍流边界层空间模式直接数值模拟中入口条件的研究

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应用技术

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飞行器典型流场转捩和湍流结构的数值研究

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高超声速流动的转捩和湍流研究

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航空航天飞行器中考虑非平行流的转捩预测方法的研究

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应用技术

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应用技术

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应用技术

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惰性气体灭火系统喷嘴流量特性的数值仿真技术咨询

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与超声速/高超声速飞行器有关的边界层转捩预测方法及湍流计算的研究

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亚、跨声速下结构/气动参数与离心叶轮顶隙涡流耦合机理的研究

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应用技术

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应用技术

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面向工程的可压缩边界层转捩预测软件的开发

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应用技术

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第十届全国流体力学青年研讨会

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应用技术

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应用技术

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应用技术

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应用技术

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应用技术

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面向工程的可压缩边界层转捩预测软件的开发

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第十届全国流体力学青年研讨会

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跨音速叶轮内叶片型线对激波发生位置影响的直接数值模拟

On non-parallel-flow effects on boundary-layer instability: a non-perturbative approach based on local expansion

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The effect of local steady suction on the stability and transition of boundary layer on a flat plate

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Numerical Investigation of Positive Displacement Blower with Countercurrent Cooling Technique

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Non-parallel-flow effect on compressible boundary layer on a flat plate

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A local scattering approach for the effect of abrupt changes on boundary-layer instability and transition: a numerical method

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Inflow boundary conditions for DNS of compressible turbulent boundary layers

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Instability analysis and transition prediction on a swept RAE2822 airfoil with constant lift coefficient

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A local scattering approach for the effects of abrupt changes on boundary-layer instability and transition: A finite-Reynolds

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第十届全国流体力学青年研讨会简介

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Instability Analysis and Drag Coefficient Prediction on a Swept RAE2822 Wing with Constant Lift Coefficient

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A non-perturbative approach to spatial instability of weakly non-parallel shear flows

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Effect of attack angle on stability and transition in a swept-wing boundary layer

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Effect of sweep angle on stability and transition in a swept-wing boundary layer

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Effect of local hump on stability of compressible boundary layer on flat plate

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A local scattering approach to study the instability of boundary layers for local scattering problem

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机翼边界层的横流稳定性分析和转捩预测

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Application of inflow boundary conditions for DNS on bypass transition

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Numerical study of a positive displacement blower

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Realization of automated face-mesh linking in GAMBIT based on journal file technique

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Inflow conditions for spatial direct numerical simulation of turbulent boundary layers

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Inflow conditions for spatial direct numerical simulation of turbulent boundary layers

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面链接自动化的实现与应用

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入口非均匀性对离心压缩机级性能影响的数值分析

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The investigation of coherent structures in the wall region of a supersonic turbulent boundary layer based on DNS database

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Study of mechanism of breakdown in laminar-turbulent transition of supersonic boundary layer on flat plate

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The mechanism of breakdown in laminar-turbulent transition of a supersonic boundary layer on a flat plate-temporal mode

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Direct numerical simulation of a supersonic turbulent boundary layer on a flat plate and its analysis.

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Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets

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壁湍流标度律的实验研究