We report on an experimental investigation on the effect of sinusoidal riblets on the near-wall characteristics of a turbulent boundary layer. The investigated riblets are characterized by a fixed wavelength and two different values of the amplitude. We comment on the flow field organization via hot wire anemometry, planar and stereoscopic particle image velocimetry experiments; furthermore, we infer on the friction drag, directly measured with a load cell, comparing the sinusoidal riblets to the reference case of riblets aligned with the mean flow (longitudinal riblets) and the Smooth case.We show that the sinusoidal riblets generally yield higher drag reduction, attaining values as large as 10%, compared with the longitudinal riblets that...
Present research has concluded that a structured rough surface has potential drag reduction performa...
Results of viscous drag reduction using 3M riblets on a NACA 0012 airfoil model up to moderate angle...
Results of viscous drag reduction using riblets from 3M on a NACA 0012 airfoil model up to moderate ...
We experimentally investigate the effects of microgrooves on the development of a zero pressure grad...
Drag reduction in wall-bounded flows can be achieved by the passive flow control technique, riblets....
Data availability: Data will be made available on request.Copyright © 2022 The Authors. A feasibilit...
© 2020 Sebastian EndrikatFlow passing over the surface of vehicles creates significant skin-friction...
The purpose of this thesis is to give answer to the question: why do riblets stop working for a cert...
A long-standing question in riblet research is why drag reduction only occurs within a small, non-di...
The interaction of the overlying turbulent flow with riblets, and its impact on their drag reductio...
Control of laminar-turbulent transition in boundary layers is one of key technologies to reduce aero...
A very important research effort has been developed at many world laboratories these last years in o...
首都大学東京博士(工学)Control of laminar-turbulent transition in boundary layers is one of key technologies to...
Vortical structure in wall turbulence over a sinusoidal riblet surface is investigated by means of a...
Present research has concluded that a structured rough surface has potential drag reduction performa...
Present research has concluded that a structured rough surface has potential drag reduction performa...
Results of viscous drag reduction using 3M riblets on a NACA 0012 airfoil model up to moderate angle...
Results of viscous drag reduction using riblets from 3M on a NACA 0012 airfoil model up to moderate ...
We experimentally investigate the effects of microgrooves on the development of a zero pressure grad...
Drag reduction in wall-bounded flows can be achieved by the passive flow control technique, riblets....
Data availability: Data will be made available on request.Copyright © 2022 The Authors. A feasibilit...
© 2020 Sebastian EndrikatFlow passing over the surface of vehicles creates significant skin-friction...
The purpose of this thesis is to give answer to the question: why do riblets stop working for a cert...
A long-standing question in riblet research is why drag reduction only occurs within a small, non-di...
The interaction of the overlying turbulent flow with riblets, and its impact on their drag reductio...
Control of laminar-turbulent transition in boundary layers is one of key technologies to reduce aero...
A very important research effort has been developed at many world laboratories these last years in o...
首都大学東京博士(工学)Control of laminar-turbulent transition in boundary layers is one of key technologies to...
Vortical structure in wall turbulence over a sinusoidal riblet surface is investigated by means of a...
Present research has concluded that a structured rough surface has potential drag reduction performa...
Present research has concluded that a structured rough surface has potential drag reduction performa...
Results of viscous drag reduction using 3M riblets on a NACA 0012 airfoil model up to moderate angle...
Results of viscous drag reduction using riblets from 3M on a NACA 0012 airfoil model up to moderate ...