首页> 外文会议>IUTAM Symposium on One Hundred Years of Boundary Layer Research >BOUNDARY-LAYER INSTABILITY IN TRANSONIC RANGE OF VELOCITIES, WITH EMPHASIS ON UPSTREAM ADVANCING WAVE PACKETS
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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 Ma > 1 is resolved by discovering a new unstable eigenmode 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 dispeision 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:对于高亚音速和低超音速来开发广义的三角形方法,假设雷诺数RE为大约是长度的悖论,围绕由MA> 1的三角形的经典版本预测的边界层稳定性是通过发现解决的一种新的不稳定特征模型,在跨音质相似度参数的一些临界值下出现的凹凸螺旋叶片涡流的频率和两个波数在缩放变量中显示为渐近变量,与着名的相似类型的不可压缩关系相同的解除关系Prandtl [1]介绍的边界层方程[1]一个世纪前的扩展理论。

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