Results 111 to 120 of about 8,410 (226)

A simulation and experimental study of a valveless piezoelectric micropump based on the synthetic jet principle

open access: yesNanotechnology and Precision Engineering
A stacked piezoelectric micropump based on the synthetic jet principle with a size of 22 × 22 × 5 mm3 is designed and fabricated. Through theoretical and finite element method (FEM) analysis, the conditions for achieving a synthetic jet structure are ...
Wencheng Lv   +8 more
doaj   +1 more source

Multi-field coupled simulation and structural design of piezoelectric synthetic jet actuator

open access: yesAIP Advances
Piezoelectric synthetic jet actuators can generate a certain amount of thrust by generating a non-constant vortex ring jet at the nozzle. It does not have a motor or rotor, which makes it advantageous and provides significant advantages in areas such as ...
Lei Song   +4 more
doaj   +1 more source

Unsteady Simulation of a Synthetic Jet Actuator with Cylindrical Cavity Using a 3-D Lattice Boltzmann Method

open access: yesInternational Journal of Aerospace Engineering, 2018
A synthetic jet actuator is a zero-net mass-flux device that imparts momentum to its surroundings and has proved to be a useful active flow control device.
Hongbin Mu   +3 more
doaj   +1 more source

Three-dimensional Flow Field Characteristics of a Normal Slot Plasma Synthetic Jet Actuator [PDF]

open access: yesJournal of Applied Fluid Mechanics
In this work, to comprehensively analyze the flow field characteristics of a normal slot plasma synthetic jet actuator, three-dimensional simulation models are established for both normal slot and normal orifice actuators. A detailed comparative analysis
L. Cheng, X. L. Sun, S. Ma
doaj   +1 more source

Maximization of integral outlet quantities of an axisymmetric synthetic jet actuator based on a loudspeaker

open access: yesEPJ Web of Conferences, 2016
The goal of this paper is to find an optimal nozzle size of an axisymmetric synthetic jet actuator based on a loudspeaker. The desirable maximized output quantities are: volumetric flow, momentum flux, and kinetic energy flux.
Kordík J., Trávníček Z.
doaj   +1 more source

Turbulence Measurements on a 2D NACA 0036 with Synthetic Jet Flow Control [PDF]

open access: yes, 2006
An active flow control experiment was conducted on a 2-ft chord NACA 0036 airfoil in a 3-ft by 4-ft Wind Tunnel at Re = 1 x 10(exp 6). The model was equipped with synthetic jet actuators at x/c = 0.30 and 0.65 that provided 120 Hz periodic excitation at ...
Wilson, J. S.
core   +1 more source

Experimental Study on the Characteristics of Dual Synthetic Jets Modulated by Driving Signals

open access: yesActuators
Piezoelectric synthetic jet actuators typically struggle to generate high-speed jets at low driving frequencies due to the coupling effect between jet frequency and jet intensity. This limitation to some extent restricts their application in flow control
Shiqing Li   +3 more
doaj   +1 more source

Design Optimization Tool for Synthetic Jet Actuators Using Lumped Element Modeling [PDF]

open access: yes
The performance specifications of any actuator are quantified in terms of an exhaustive list of parameters such as bandwidth, output control authority, etc.
Cattafesta, Louis N., III   +3 more
core   +1 more source

Flow Control Applications [PDF]

open access: yes
Flow control has a long history with many successes across a plethora of applications. This report addresses the characteristics of the approaches that are actually used, why they are used, the many approaches that are not used, and why.
Bushnell, Dennis M., Wygnanski, Israel
core   +1 more source

Numerical Study of Flow Separation Control over a Hump Airfoil Using a Novel Sweeping Jet Actuator

open access: yesApplied Sciences
Sweeping jet (SWJ) actuators have become a hot research topic in flow control due to their larger sweep range and higher control efficiency. However, the linear relationship between frequency and velocity ratio (VR = Ujet/U∞) in the SWJ actuator makes it
Tong Zhao, Yalei Bai
doaj   +1 more source

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