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Boundary-Layer Instability in Transonic Range of Velocities, with Emphasis on Upstream Advancing Wave Packets

机译:跨音速范围内的边界层不稳定性,重点在上游推进波包上

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A generalized triple-deck approach is developed for high subsonic and low supersonic velocities, assuming the Reynolds number Re to be large. A longstanding paradox about the boundary-layer stability predicted by the classical version of the triple deck for M_(infinity) > 1 is resolved by discovering a new unstable eigemnode that emerges at some critical value of a transonic similarity parameter. The frequency and both wavenumbers of unsteady spiral Gortler vortices on a concave surface are shown to asymptotically obey in scaled variables the same dispersion relation as incompressible disturbances of a similar type. The famous boundary-layer equations introduced by Prandtl [1] a century ago underlie the extended theory.
机译:假设雷诺数RE为大的高亚音图和低超音速,开发了广义的三角形方法。通过发现在跨音相似度参数的一些临界值中出现的新不稳定的Eigemeode来解析关于M_(Infinity)> 1的三层(Infinity)> 1的经典版本预测的边界层稳定性的长期悖论。在凹面上的不稳定螺旋Gorter涡流的频率和两个波数显示在缩放变量中的渐近性遵循与类似类型的不可压缩的扰动相同的色散关系。 Prandtl [1]介绍的着名边界层方程[1]一个世纪前的扩展理论。

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