Three-dimensional effect on transonic rectangular cavity flows

被引:19
作者
Chung, KM [1 ]
机构
[1] Natl Cheng Kung Univ, Aerosp Sci & Technol Res Ctr, Tainan 711, Taiwan
关键词
Vortex; Pressure Gradient; Mach Number; Surface Pressure; Peak Pressure;
D O I
10.1007/s003480000232
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Experiments are performed to study the characteristics of rectangular cavity flows. Mean and fluctuating surface pressures in a Mach 1.28 turbulent flow past rectangular cavities are obtained. The cavity length-to-depth ratio (L/D) is varied from 2.43 to 43.00, while the length-to-width ratio (L/W) is 0.5, 1.0 and 2.0. The three-dimensional effect is significant on the trailing edge vortex, which affects the peak pressure ahead of the rear face, pressure gradient and levels of pressure fluctuation near the trailing edge, particularly for closed and transitional cavity flows. L/W and Mach number are important for the definition of critical LID for the cavity flowfield models.
引用
收藏
页码:531 / 536
页数:6
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