机译:用均匀吹割的高雷诺数的湍流边界层的实验研究,I I:统计
Brandenburg Univ Technol Cottbus Senftenberg Dept Aerodynam &
Fluid Mech Siemens Halske Ring 14 D-03046 Cottbus Germany;
Brandenburg Univ Technol Cottbus Senftenberg Dept Aerodynam &
Fluid Mech Siemens Halske Ring 14 D-03046 Cottbus Germany;
Univ Lille FRE 2017 LMFL Lab Mecan Fluides Lille Kampe Ferie Cent Lille CNRS ONERA Arts &
Metiers ParisTech Lille France;
Brandenburg Univ Technol Cottbus Senftenberg Dept Aerodynam &
Fluid Mech Siemens Halske Ring 14 D-03046 Cottbus Germany;
Univ Lille FRE 2017 LMFL Lab Mecan Fluides Lille Kampe Ferie Cent Lille CNRS ONERA Arts &
Metiers ParisTech Lille France;
Brandenburg Univ Technol Cottbus Senftenberg Dept Aerodynam &
Fluid Mech Siemens Halske Ring 14 D-03046 Cottbus Germany;
Turbulent boundary layers; drag reduction; flow control; particle image velocimetry; uniform blowing;
机译:用均匀吹割的高雷诺数的湍流边界层的实验研究,I I:统计
机译:雷诺数对湍流边界层结构吸力影响的实验研究
机译:均匀吹风或吸力对高超声速的空间发展湍流边界层的影响
机译:极高雷诺数下上游条件对光滑和粗糙零压力梯度湍流边界层流动影响的实验研究
机译:高雷诺数湍流边界层的实验研究。
机译:湍流边界层中层级和尺度相互作用的雷诺数趋势
机译:多孔板上的湍流边界层-实验性传热,具有均匀的吹气和吸力,并具有中等强度的加速度