高超声速边界层的转捩及预测

doi:10.7527/S1000-6893.2014.0244

Abstract

Abstract:

It is summarized that the basic process and problems of the transition of boundary layers. Based on which, the fundamentally distinguishes in instability of hypersonic boundary layers from incompressible boundary layers are shown, and the transition mechanism, receptivity characteristic, transition prediction methods for three-dimensional hypersonic boundary layers are introduced, in which the e^N method using in engineering and it's rational improvement is specially shown. Some application examples of prediction transition for three-dimensional hypersonic boundary layers using e^N method are given. Finally, the difficulty and problems need to be solved in the hypersonic boundary layers are introduced.

Key words: hypersonic boundary layer, hydrodynamic stability theory, mechanism and prediction of transition, receptivity, e^N method

CLC Number:

LUO Jisheng. Transition and prediction for hypersonic boundary layers[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 357-372.

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Transition and prediction for hypersonic boundary layers

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