Towards in-flight applications? A review on dielectric barrier discharge-based boundary-layer control

J Kriegseis, B Simon… - Applied …, 2016 - asmedigitalcollection.asme.org
Active control of laminar boundary layers with dielectric barrier discharge (DBD) plasma
actuators (PAs) has made considerable progress in the last 15 years. First pioneering …

Identification and mitigation of TS waves using localized dynamic surface modification

M Amitay, BA Tuna, H Dell'Orso - Physics of Fluids, 2016 - pubs.aip.org
The control of transition from a laminar to a turbulent flow over a flat plate using localized
dynamic surface modifications was explored experimentally in Rensselaer Polytechnic …

Thermal performance of microelectronic substrates with submillimeter integrated vapor chamber

S Cho, Y Joshi - Journal of Heat Transfer, 2019 - asmedigitalcollection.asme.org
We develop a vapor chamber integrated with a microelectronic packaging substrate and
characterize its heat transfer performance. A prototype of vapor chamber integrated printed …

Cancellation of Tollmien–Schlichting waves in direct vicinity of a plasma actuator

B Simon, D Markus, C Tropea, S Grundmann - AIAA Journal, 2018 - arc.aiaa.org
The active cancellation of Tollmien–Schlichting waves is a promising and energy-efficient
laminar flow control technology with the goal of drag reduction by delaying laminar …

Investigation of the effect of inlet turbulence and Reynolds number on developing duct flow

BA Tuna, S Yarusevych, X Li… - Journal of Fluids …, 2019 - asmedigitalcollection.asme.org
This study investigates experimentally the effects of upstream flow conditions and Reynolds
number on a developing duct flow. Particle image velocimetry (PIV) and hot-wire (HW) …

Investigation of the effect of inlet turbulence on transitional wall-bounded flows

BA Tuna, X Li, S Yarusevych - Fluids …, 2017 - asmedigitalcollection.asme.org
The present work investigates experimentally the effects of grid-generated turbulence on the
transition and the hydrodynamic entrance length in a developing duct flow. Particle Image …

Active cancellation of Tollmien-Schlichting waves under varying inflow conditions for in-flight application

BJ Simon - 2017 - tuprints.ulb.tu-darmstadt.de
Active flow control in laminar boundary layers can reduce wall friction on a wing, if laminar-
turbulent transition is delayed. In this thesis,(re-) active flow control for active cancellation of …

[PDF][PDF] Investigation of the Effect of Inlet Turbulence and Reynolds Number on Developing Duct Flow

X Li, Y Ren, F Shi - researchgate.net
This study investigates experimentally the effects of upstream flow conditions and Reynolds
number on a developing duct flow. Particle image velocimetry (PIV) and hotwire (HW) …

[PDF][PDF] Evaporation of Lubricant Films Subjected to Laminar and Turbulent Boundary Layers

S Yarusevych, X Li, F Shi - researchgate.net
This work investigates experimentally the effects of grid-generated turbulence on the
evaporation of thin oil films subjected to laminar, transitional, and turbulent boundary layers …

Evaporation of Lubricant Films Subjected to Laminar and Turbulent Boundary Layers

SJ Gill, BA Tuna, S Yarusevych… - Journal of Fluids …, 2020 - asmedigitalcollection.asme.org
This work investigates experimentally the effects of grid-generated turbulence on the
evaporation of thin oil films subjected to laminar, transitional, and turbulent boundary layers …