Laminar boundary layer stability calculation for contoured Mach 6 nozzle

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

Original language	English
Pages (from-to)	35-44
Number of pages	10
Journal	Thermophysics and Aeromechanics
Volume	27
Issue number	1
DOIs	https://doi.org/10.1134/S0869864320010035
Publication status	Published - 1 Jan 2020

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

ID: 24261562