Experiments on the Artificial Disturbance Evolution in 2D and 3D Spanwise Modulated Boundary Layers at Mach 2 and 2.5

Original language	English
Pages (from-to)	48-57
Number of pages	10
Journal	Procedia IUTAM
Volume	14
DOIs	https://doi.org/10.1016/j.piutam.2015.03.023
Publication status	Published - 2015
Event	8th IUTAM-ABCM Symposium on Laminar Turbulent Transition, LTT 2014 - Rio de Janeiro, Brazil Duration: 8 Sept 2014 → 12 Sept 2014

artificial disturbance, boundary layer, experiments, flat palate, laminar-turbulent transition, microroughness, nonlinearity, supersonic flow, swept wing

ID: 25840700