Linear stability of supersonic boundary layer over a cooled porous surface

Alexey Kudryavtsev, Dmitry Khotyanovsky

Результат исследования: Научные публикации в периодических изданияхстатья по материалам конференции

Аннотация

The linear stability of the boundary layer at high supersonic Mach numbers on a flat plate with a cooled porous surface is studied. As is well known, at high supersonic speeds, both vortex disturbances of the first mode and acoustic disturbances of the second mode are unstable. The more unstable disturbances of the second mode can be stabilized using sound-absorbing porous coatings. At the same time, such coatings have a destabilizing effect on the disturbances of the first mode. Surface cooling is one of the factors potentially capable of preventing such a destabilization. Based on this assumption, in the present work, the linear theory of stability is used to consider the combined effect of a sound-absorbing coating and surface cooling.

Язык оригиналаанглийский
Номер статьи012114
ЖурналJournal of Physics: Conference Series
Том1404
Номер выпуска1
DOI
СостояниеОпубликовано - 6 дек 2019
Событие16th All-Russian Seminar with International Participation on Dynamics of Multiphase Media, DMM 2019 - Novosibirsk, Российская Федерация
Продолжительность: 30 сен 20195 окт 2019

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