scholarly journals Synthetic Jet Flow Field Database for CFD Validation

Author(s):  
Chungsheng Yao ◽  
Fang-Jenq Chen ◽  
Jerome Harris ◽  
Dan Neuhart
2005 ◽  
Author(s):  
Paul D. Orkwis ◽  
Matteo Pes ◽  
Claudio Filz ◽  
Terry Daviaux ◽  
Katherine Grendell ◽  
...  
Keyword(s):  
Jet Flow ◽  

2004 ◽  
Vol 28 (4) ◽  
pp. 265-272 ◽  
Author(s):  
S.G. Mallinson ◽  
J.A. Reizes ◽  
G. Hong ◽  
P.S. Westbury

1991 ◽  
Vol 18 (1) ◽  
pp. 1-9
Author(s):  
E. Rathakrishnan ◽  
T.J. Ignatius ◽  
Channa Raju

Author(s):  
Pushpanjay K. Singh ◽  
M. Renganathan ◽  
Harekrishna Yadav ◽  
Santosh K. Sahu ◽  
Prabhat K. Upadhyay ◽  
...  

2010 ◽  
Vol 37 (8) ◽  
pp. 2098-2103
Author(s):  
易德先 Yi Dexian ◽  
胡芳友 Hu Fangyou ◽  
赵维义 Zhao Weiyi ◽  
崔爱永 Cui Aiyong ◽  
卢长亮 Lu Changliang

2015 ◽  
Vol 27 (2) ◽  
pp. 181-190 ◽  
Author(s):  
Haifu Wang ◽  
Liangcai Cai ◽  
Xiaolei Chong ◽  
Hao Geng

A combined blast fence is introduced in this paper to improve the solid blast fences and louvered ones. Experiments of the jet engine exhaust flow (hereinafter jet flow for short) field and tests of three kinds of blast fences in two positions were carried out. The results show that the pressure and temperature at the centre of the jet flow decrease gradually as the flow moves farther away from the nozzle. The pressure falls fast with the maximum rate of 41.7%. The dynamic pressure 150 m away from the nozzle could reach 58.8 Pa, with a corresponding wind velocity of 10 m/s. The temperature affected range of 40°C is 113.5×20 m. The combined blast fence not only reduces the pressure of the flow in front of it but also solves the problems that the turbulence is too strong behind the solid blast fences and the pressure is too high behind the louvered blast fences. And the pressure behind combined blast fence is less than 10 Pa. The height of the fence is related to the distance from the jet nozzle. The nearer the fence is to the nozzle, the higher it is. When it is farther from the nozzle, its height can be lowered.


2006 ◽  
Vol 110 (1108) ◽  
pp. 385-393 ◽  
Author(s):  
M. Jabbal ◽  
J. Wu ◽  
S. Zhong

AbstractPIV measurements in the near-field region of a jet flow emanating from a round synthetic jet actuator into quiescent air were conducted over a range of operating conditions. The primary purpose of this work was to investigate the nature of synthetic jets at different operating conditions and to examine the jet flow parameters that dictate the behaviour of synthetic jet actuators. The effects of varying diaphragm displacement and oscillatory frequency for fixed actuator geometry were studied. It was observed that the characteristics of synthetic jets are largely determined by the Reynolds number and stroke length. An increase in the former is observed to increase the strength of consecutive vortex rings that compose a synthetic jet, whereas an increase in the latter results in an increase in relative vortex ring spacing and for further increases in stroke length, shedding of secondary vortices. Correlations were also made between the operating parameters and the performance parameters most effective for flow control and which therefore determine the impact of a synthetic jet on an external flow. Relations of time-averaged dimensionless mass flux, momentum flux and circulation with the jet flow conditions were established and found to widely support an analytical performance prediction model described in this paper. It is anticipated that the experimental data obtained in this study will also contribute towards providing a PIV database for macro-scale synthetic jet actuators.


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