高超声速边界层的转捩及预测
收稿日期: 2014-08-04
修回日期: 2014-10-08
网络出版日期: 2014-10-09
基金资助
国家自然科学基金 (11332007)
Transition and prediction for hypersonic boundary layers
Received date: 2014-08-04
Revised date: 2014-10-08
Online published: 2014-10-09
Supported by
National Natural Science Foundation of China (11332007)
罗纪生 . 高超声速边界层的转捩及预测[J]. 航空学报, 2015 , 36(1) : 357 -372 . DOI: 10.7527/S1000-6893.2014.0244
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 eN 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 eN method are given. Finally, the difficulty and problems need to be solved in the hypersonic boundary layers are introduced.
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