Effect of unit Reynolds number on the laminar-turbulent transition on a swept wing in supersonic flow

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

Original language	English
Pages (from-to)	659-665
Number of pages	7
Journal	Thermophysics and Aeromechanics
Volume	25
Issue number	5
DOIs	https://doi.org/10.1134/S0869864318050025
Publication status	Published - 1 Sept 2018

laminar-turbulent transition, supersonic boundary layer, swept wing, unit Reynolds number, BOUNDARY-LAYER, NOISE

ID: 18144037