Author/Authors :
Nishibe, K Department of Mechanical Engineering - Tokyo City University, Setagaya, Tokyo, Japan , Nomura, Y Graduate School of Engineering - Tokyo City University, Setagaya, Tokyo, Japan , Noda, K Graduate School of Engineering - Tokyo City University, Setagaya, Tokyo, Japan , Ohue, H Department of Mechanical Engineering - Tokyo City University, Setagaya, Tokyo, Japan , Sato, K Depertment of Mechanical System Engineering - Kogakuin University, Shinjuku, Tokyo, Japan
Abstract :
Synthetic jets, whose size and weight can be reduced easily, have become an attractive alternative to continuous
jets. Many experimental and numerical studies have been conducted on synthetic jets to investigate their
fundamental flow characteristics, including jet structure, for applied research such as boundary layer control
and enhanced fluid mixing. However, few studies have focused on fluid transportation devices using synthetic
jets as a driving source. Therefore, several issues concerning fluid transport characteristics still need to be
resolved. In addition, although optimum operation of devices using synthetic jets is essential for their practical
use, few studies have focused on this issue. The present study experimentally demonstrates the influence of the
dimensionless stoke L on the performance characteristics of a synthetic jet fan under Reynolds number Re =
1800 and the same fan geometry; here, the stroke l is nondimensionalized by the primary slot width b.
Furthermore, numerical simulations are conducted to complement the experiment. Velocity and pressure
measurements are performed using a hot-wire anemometer, differential pressure manometer, and pressure
transducer. The influence of the dimensionless stroke L on the performance/efficiency curves, static pressure
distribution on the duct surface, and unsteady flow characteristics are investigated. Moreover, the flow field
inside the duct is observed through numerical simulation. The results show that the performance characteristics
and pressure recovery process depend on the dimensionless stroke L, and an optimum range of dimensionless
stroke L exists for operation.
Keywords :
Pressure recovery , Fan performance curve , Jet pump , Synthetic jets