摘要
简述了在西北工业大学低湍流度风洞中,用热线风速仪对翼型边界层及近场尾流中雷诺正应力及切应力等的测量结果,着重讨论了雷诺切应力及湍流动能的分布规律及相关特性。结果表明,各区段的相关规律并不相同,与常规结果有明显差异。
This paper describes the velocity profile, turbulence intensity and Reynolds stress in the boundary layer and near wake of an airfoil measured in the low turbulence wind tunnel of NPU using a DISA hot wire anemometer. The distribution of Reynolds shear stress and turbulent kinetic energy was described and the correlation of these two quantities was discussed.It has shown, the correlation is different at different y position and is different from the correlation at ordinary turbulence level.
出处
《空气动力学学报》
CSCD
北大核心
1997年第2期220-225,共6页
Acta Aerodynamica Sinica
基金
航空科学基金
关键词
翼型
边界层
近场尾流
切应力
湍流动能
low turbulence
airfoil, boundary layer
near wake
turbulent shear stress
turbulent kinetic energy