Investigation of the influence of a local change in surface temperature on the laminar boundary layer stability in a hypersonic nozzle

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

Original language	English
Pages (from-to)	633-642
Number of pages	10
Journal	Thermophysics and Aeromechanics
Volume	27
Issue number	5
DOIs	https://doi.org/10.1134/S0869864320050017
Publication status	Published - Sept 2020

boundary layer, Goertler vortices, hypersonic nozzle, laminar-turbulent transition, linear stability theory, local heating

ID: 27890340