Recent theoretical, numerical, and experimental investigations performed at the Department of Mechanics, KTH Stockholm, and the Department of Mechanical Engineering, Eindhoven …
Detailed comparison of spatial direct numerical simulations (DNS) and secondary linear stability theory (SLST) is provided for the three-dimensional crossflow-dominated boundary …
CY Schuele, TC Corke, E Matlis - Journal of Fluid Mechanics, 2013 - cambridge.org
Spanwise-periodic roughness designed to excite selected wavelengths of stationary cross- flow modes was investigated in a three-dimensional boundary layer at Mach 3.5. The test …
An experimental investigation of primary and secondary crossflow instability developing in the boundary layer of a is presented. Linear stability theory is applied for preliminary …
T Corke, A Arndt, E Matlis, M Semper - Journal of Fluid Mechanics, 2018 - cambridge.org
Experiments were performed to investigate passive discrete roughness for transition control on a sharp right-circular cone at an angle of attack at Mach 6.0. A cone angle of attack of …
Experiments have been conducted on a swept wing model in a low-turbulence wind tunnel at chord Reynolds number of to investigate the unsteady interaction of a forward-facing step …
This paper describes a detailed experimental study using hot-wire anemometry of the laminar–turbulent transition region of a rotating-disk boundary-layer flow without any …
G Zoppini, D Ragni, M Kotsonis - Physics of Fluids, 2022 - pubs.aip.org
The present work is dedicated to the investigation of the effect of an isolated roughness element on a swept wing boundary layer. In particular, the flow modifications incurred by a …