Microscale combustion: Technology development and fundamental research

Y Ju, K Maruta - Progress in energy and combustion science, 2011 - Elsevier
The high energy density of hydrocarbon fuels creates a great opportunity to develop
combustion based micro-power generation systems to meet increasing demands for …

Comparison of DBD plasma actuators flow control authority in different modes of actuation

M Abdollahzadeh, JC Pascoa, PJ Oliveira - Aerospace science and …, 2018 - Elsevier
The principal mechanisms by which DBD plasma actuators influence flow characteristics,
and are thus able to control that flow, depend strongly on their modes of actuation. Here two …

Dielectric barrier discharge flow control at very low flight Reynolds numbers

D Greenblatt, B Goksel, I Rechenberg, CY Schule… - AIAA journal, 2008 - arc.aiaa.org
ACHIEVING sustained flight of micro air vehicles (MAVs) brings significant challenges due to
their small dimensions and lowflight speeds [1]. For so-called mini air vehicles, which …

[图书][B] Fundamentals and applications of modern flow control

RD Joslin, DN Miller - 2009 - arc.aiaa.org
Flow control technologies have been used in the past century to control fluid flows. This text
presents the current state of the art in emerging modern flow control technologies and …

Effects of duty cycles of the plasma actuators on improvement of pressure distribution above a NLF0414 airfoil

AS Taleghani, A Shadaram… - IEEE Transactions on …, 2012 - ieeexplore.ieee.org
This paper investigates the effects of duty cycle on improvement of pressure distribution
above a NLF0414 airfoil using the plasma actuators. Three dielectric barrier discharges as …

Numerical and experimental investigation on the flow separation control of S809 airfoil with slot

Y Xie, J Chen, H Qu, G Xie, D Zhang… - Mathematical …, 2013 - Wiley Online Library
A new flow control approach called split blade is applied on the S809 airfoil in the present
study. S809 airfoil was investigated experimentally and numerically with different operating …

Plasma actuation effect on a NACA 4412 airfoil

B Karadag, C Kolbakir, AS Durna - Aircraft Engineering and …, 2021 - emerald.com
Purpose This paper aims to investigate the effects of a dielectric barrier discharge (DBD)
plasma actuator (PA) qualitatively on aerodynamic characteristics of a 3 D-printed NACA …

Aerodynamic performance enhancements using discharge plasma actuators

D Greenblatt - US Patent 8,708,651, 2014 - Google Patents
B64C II/IS(2006.01)(57) ABSTRACT F4D 29/38(2006.01) The current invention provides
significant performance (52) US Cl. improvements or significant energy savings for fans …

Experimental study on dielectric barrier discharge actuators operating in pulse mode

M Kotsonis, L Veldhuis - Journal of Applied Physics, 2010 - pubs.aip.org
An experimental investigation is performed on the operation of dielectric barrier discharge
plasma actuators used as manipulators of secondary and unsteady flow structures such as …

A Numerical Study on the Influence of Transverse Grooves on the Aerodynamic Performance of Micro Air Vehicles Airfoils

Z Li, Y Zuo, H Zhang, L He, E Sun, Y Long, L Zhang… - Applied Sciences, 2023 - mdpi.com
Micro Air Vehicles (MAVs) airfoils usually operate at low Reynolds number conditions,
where viscous drag will consume a large amount of propulsion power. Due to the small …