Computational study on the effect of orifice-edge-chamfered angle on the synthetic jet characteristics Online publication date: Wed, 27-Nov-2019
by Hong Mun Hoh; Cheng See Yuan; Teo Yong Soon; Lim Kim Chuan
International Journal of Engineering Systems Modelling and Simulation (IJESMS), Vol. 11, No. 3, 2019
Abstract: The effect of chamfered orifice edges on the time-averaged pressure difference and jet velocity of synthetic jet have been numerically investigated. Chamfered orifice edges with exit angle of 15° and 30° are analysed. Moving grid is utilised to define the moving diaphragm of the actuator. The results are validated against experimental data. The time-averaged pressure difference between the location inside the orifice duct and downstream region where the velocity becomes negligible have been numerically predicted for all the cases. The jet velocity is predicted numerically at the downstream location of 1 mm from the orifice exit. The overall results indicated that the changes of chamfered orifice edges give significant impact on the time-averaged pressure difference. The jet velocity is also affected by the variation of the chamfer orifice edges during the expulsion stage. The findings from this study provides a basic design guideline for designing a synthetic jet actuator with lower minor loss and power dissipation.
Existing subscribers:
Go to Inderscience Online Journals to access the Full Text of this article.
If you are not a subscriber and you just want to read the full contents of this article, buy online access here.Complimentary Subscribers, Editors or Members of the Editorial Board of the International Journal of Engineering Systems Modelling and Simulation (IJESMS):
Login with your Inderscience username and password:
Want to subscribe?
A subscription gives you complete access to all articles in the current issue, as well as to all articles in the previous three years (where applicable). See our Orders page to subscribe.
If you still need assistance, please email subs@inderscience.com