Linear development of controlled disturbances in the supersonic boundary layer on a swept wing at Mach 2 › Research Explorer

Novosibirsk State University's Research Portal

Linear development of controlled disturbances in the supersonic boundary layer on a swept wing at Mach 2

Research output: Contribution to journal › Article › peer-review

General Physics Section

DOI

https://doi.org/10.1063/1.4952999
Final published version

A. D. Kosinov
G. L. Kolosov
N. V. Semionov
Yu G. Yermolaev

Original language	English
Article number	064101
Journal	Physics of Fluids
Volume	28
Issue number	6
DOIs	https://doi.org/10.1063/1.4952999
Publication status	Published - 1 Jun 2016

OECD FOS+WOS

ID: 25838761