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超声速边界层中小幅值T-S波的数值研究
A Numerical Study for Small Amplitude T-S Waves in a Supersonic Boundary Layer
【摘要】 对来流马赫数Ma∞ =4 5的平板边界层中 ,幅值A分别为来流速度的 0 0 1,0 0 0 1,0 0 0 0 1倍的扰动波传播的物理过程进行了直接数值模拟· 计算采用 NND格式· 模拟中发现即使扰动幅值尚小时 ,流场中即已出现小激波·
【Abstract】 The propagation of the disturbance waves in a boundary layer at Mach number=4 5 is studied by direct numerical simulation (DNS), using NND scheme, and different amplitudes A=0 01,0 001,0 000 1 of the disturbance have been assumed. The numerical result shows that there might be shocklets induced in the boundary layer, even when the amplitude of disturbance wave is still small.
【关键词】 直接数值模拟;
小激波;
可压缩边界层;
【Key words】 direct numerical simulation; shocklet; compressible boundary layerH;
【Key words】 direct numerical simulation; shocklet; compressible boundary layerH;
【基金】 国家95攀登计划资助项目!(19732 0 0 5)
- 【文献出处】 应用数学和力学 ,Applied Mathematics and Mechanics , 编辑部邮箱 ,2000年12期
- 【被引频次】7
- 【下载频次】101