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Investigation of the effect of heavy gas injection into a supersonic boundary layer on laminar-turbulent transition

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

DOI

https://doi.org/10.1134/S0015462817060052
Final published version

S. A. Gaponov
Yu G. Ermolaev
N. N. Zubkov
A. D. Kosinov
V. I. Lysenko
B. V. Smorodskii
A. A. Yatskikh

Original language	English
Pages (from-to)	769-776
Number of pages	8
Journal	Fluid Dynamics
Volume	52
Issue number	6
DOIs	https://doi.org/10.1134/S0015462817060052
Publication status	Published - 1 Nov 2017
Externally published	Yes

Research areas

compressible boundary layer, hydrodynamic stability, injection, laminar-turbulent transition, permeable surface, PERMEABILITY, STABILITY, ROUGHNESS

OECD FOS+WOS

ID: 25837911