1 | Consequently, secondary instability is unlikely the main cause leading to transition in supersonic boundary layers. | |
2 | In this paper, the laminar-turbulent transition and the role of transition in turbomachinery are also preliminarily discussed. | |
3 | This is consistent with the experimental results of pressure distribution and indicates that sublimation method can correctly display the transition location. | |
4 | It was tested in the prediction of the location of transition for compressible boundary layers on flat plates, and the results were compared with those obtained by direct numerical simulations(DNS). |