@inproceedings{9a7a6f08695f451b8878b725878f822c,
title = "On mechanisms of the action of weak shock waves on laminar-turbulent transition in supersonic boundary layer",
abstract = "Origin of the streaks is examined in the flat plate boundary layer at Mach 2. They arise due to the interaction of the weak shock waves with flow in vicinity of the flat plate leading edge. The process is accompanied by significant increase of the pulsation amplitudes in the boundary layer. The effect for the sharp leading edge is not so visible. The case of flat plate with blunted leading edge of 0.6 mm in radius is tested here. Results of the action of pair weak shock waves can be different and this finding is considered in the paper.",
keywords = "NOISE",
author = "Kosinov, {A. D.} and Yatskikh, {A. A.} and Yermolaev, {Yu G.} and Semionov, {N. V.} and Kolosov, {G. L.} and Piterimova, {M. V.}",
year = "2017",
month = oct,
day = "26",
doi = "10.1063/1.5007530",
language = "English",
volume = "1893",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin",
booktitle = "Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017",
note = "25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017 ; Conference date: 05-06-2017 Through 09-06-2017",
}