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Baroclinic vortex sheet production by shocks and expansion waves

机译:冲击波和膨胀波产生斜斜涡旋片

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Vortex sheet production by shocks and expansion waves refracting at a density discontinuity was examined and compared using an analytical solution and numerical simulations. The analytical solution showed that with a small exception, vortex sheet strength is generally stronger in fast/slow shock refractions. In contrast, expansion waves generated a stronger vortex sheet in slow/fast refractions. This difference results in larger vorticity deposited by shocks in fast/slow refractions and by expansion waves in slow/fast refractions. Shock refractions become irregular and the analytical solution fails when either incident, transmitted or reflected shock, exceeded the angle limit for an attached shock. To investigate vortex sheet production outside the range of analytical solutions and to verify the applicability of the planar-interface analytical solution to a curved interface, shock refraction through a sinusoidal interface was numerically simulated in the shock frame of reference. It is found that variation in the local incidence angle along the curved interface creates pressure waves that affect the level of deposited vorticity. This contributes to the difference between predictions from local analysis and numerical computation. Furthermore, an interesting behavior of the shock and expansion wave-deposited vorticity in supersonic ramp flow was discovered. When the high- and low-density streams were swapped, while keeping the incident flow Mach numbers constant, a vortex sheet of equal magnitude but of opposite sign was generated.
机译:检查并比较了解析力和数值模拟方法对由冲击波和膨胀波在密度不连续处折射产生的涡旋片的影响。分析解决方案表明,除极少数例外,在快速/慢速冲击折射中,涡旋片强度通常都较强。相反,膨胀波在慢/快折射中产生更强的涡旋片。这种差异导致快速/慢速折射中的冲击和慢速/快速折射中的膨胀波产生更大的涡旋。当入射,透射或反射的冲击超过所附加冲击的角度限制时,冲击折射将变得不规则,并且分析解决方案将失败。为了研究分析解决方案范围之外的涡流片的产生并验证平面界面分析解决方案对弯曲界面的适用性,在参考震荡框架中对通过正弦界面的折射进行了数值模拟。发现沿弯曲界面的局部入射角的变化产生了影响沉积涡度水平的压力波。这导致了局部分析和数值计算的预测之间的差异。此外,还发现了超声速斜坡流中激波和扩展波沉积涡旋的有趣行为。当交换高密度流和低密度流时,在保持入射流马赫数不变的情况下,会生成大小相等但符号相反的涡旋片。

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