Experimental study on the working characteristics of tri-electrode plasma actuator utilizing a combination of corona and barrier discharges

A Hatamoto, K Nakai, H Nishida - Actuators, 2022 - mdpi.com
A tri-electrode plasma actuator (TED-PA), which has an additional electrode with a DC
voltage, induces jets from two facing electrodes and achieves larger thrust and higher …

Nanosecond volume discharge in the non-stationary high-speed profiled channel flow

I Znamenskaya, A Lutsky, D Tatarenkova… - Physics of …, 2023 - pubs.aip.org
The aim of the work is an experimental and numerical investigation of the interaction
between the pulse volume discharge with a high-speed flow in the rectangular profiled …

Solid-State Electroaerodynamic Uncrewed Aircraft for Near-Silent Package Delivery

AJ Brown, N Gomez-Vega, S Barrett - AIAA Aviation 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-3483. vid This paper presents the
design of two uncrewed aircraft, powered by electroaerodynamic (EAD) multistaged ducted …

The Effect of SiC-MOSFET Characteristics on the Performance of Dielectric Barrier Discharge Plasma Actuators with Two-Stroke Charge Cycle Operation

S Sato, T Yoshikawa, N Ohnishi - Actuators, 2022 - mdpi.com
The low-voltage operation of a dielectric-barrier-discharge (DBD) plasma actuator with a
simple electric circuit has the potential to put it into industrial applications. However, there is …

[HTML][HTML] Ionic wind generation through coplanar discharge: A plasma actuator without exposed electrodes

S Sato, M Sakurai, N Ohnishi - AIP Advances, 2023 - pubs.aip.org
This study demonstrates the successful induction of a unidirectional ionic wind by adding an
embedded electrode in a coplanar discharge, thus breaking the generation of a symmetrical …

Towards Practical Fixed-Wing Aircraft with Electroaerodynamic Propulsion

A Brown - 2023 - oastats.mit.edu
Electroaerodynamic (EAD) propulsion is a novel means of generating thrust via collisions
between ions and neutral molecules. EAD thrusters have no moving parts, and are therefore …

Towards Development of a Plasma Actuator without External Power Supply for Unmanned Aerial Vehicle

S SATO, N OHNISHI - Journal of Evolving Space Activities, 2023 - jstage.jst.go.jp
抄録 Towards industrial use of dielectric-barrier-discharge (DBD) plasma actuators, a
practical DBD plasma actuator system including a driving circuit assumed to equip …