Numerical Study of the Evolution of Disturbances Generated by Roughness Elements in a Supersonic Boundary Layer on a Blunted Cone

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

Original language	English
Pages (from-to)	438-450
Number of pages	13
Journal	Journal of Applied Mechanics and Technical Physics
Volume	60
Issue number	3
DOIs	https://doi.org/10.1134/S0021894419030052
Publication status	Published - 1 May 2019

blunted conical body, direct numerical simulation, distributed roughness, isolated roughness elements, laminar-turbulent transition, supersonic boundary layer, TRANSITION, INSTABILITY, STABILITY, FLOW

ID: 24413070