Hostname: page-component-cd9895bd7-lnqnp Total loading time: 0 Render date: 2024-12-23T15:07:27.095Z Has data issue: false hasContentIssue false
  • English
  • Français

Experimental Study of Flow Separation over NACA633018 Wing with Synthetic Jet Control at Low Reynolds Numbers

Published online by Cambridge University Press:  16 October 2012

C.-Y. Lin  and
F.-B. Hsiao
C.-Y. Lin
Affiliation:
Institute of Aeronautics and Astronautics, National Cheng Kung University, Tainan, Taiwan 70101, R.O.C
F.-B. Hsiao*
Affiliation:
Institute of Aeronautics and Astronautics, National Cheng Kung University, Tainan, Taiwan 70101, R.O.C
*
*Corresponding author ([email protected])
Get access

Abstract

This paper experimentally studies flow separation and aerodynamic performance of a NACA633018 wing using a series of piezoelectric-driven disks, which are located at 12% chord length from the leading edge to generate a spanwise-distributed synthetic jets to excite the passing flow. The experiment is conducted in an open-type wind tunnel with Reynolds numbers (Re) of 8 × 104 and 1.2 × 105, respectively, based on the wing chord. The oscillations of the synthetic jet actuators (SJAs) disturb the neighboring passage flow on the upper surface of the wing before the laminar separation takes place. The disturbances of energy influence the downstream development of boundary layers to eliminate or reduce the separation bubble on the upper surface of the wing. Significant lift increase and drag decrease are found at the tested Reynolds number of 8 × 104 due to the actuators excitation. Furthermore, the effect of drag also reduces dominant with increasing Reynolds number, but the increase on lift is reduced with the Reynolds number increased.

Keywords

Synthetic jetPiezoelectric-drivenReynolds numbersAerodynamic performance
Type
Articles
Information
Journal of Mechanics , Volume 29 , Issue 1 , March 2013 , pp. 45 - 52
Copyright
Copyright © The Society of Theoretical and Applied Mechanics, R.O.C. 2012

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

1. Seifert, A., Darabi, A. and Wygnanski, I., “Delay of Airfoil Stall by Periodic Excitation,” Journal of Aircraft, 33, pp. 691–698 (1996).Google Scholar
2. Neuberger, D. and Wygnanski, I., “The Use of a Vibrating Ribbon to Delay Separation on Two Dimensional Airfoils,” Proceedings of Air Force Academy Workshop on Unsteady Separated Flow, Rept. TR-88-000 (1987).Google Scholar
3. Hsiao, F. B., Liu, C. F. and Shyu, J-Y., “Control of Wall-Separated Flow by Internal Acoustic Excitation,” AIAA Journal, 28, pp. 1440–1446 (1990).Google Scholar
4. Pierce, A. D., Acoustics, 1st Edition, McGraw-Hill, New York, pp. 330–333 (1981).Google Scholar
5. Chanaud, R. C., “Effects of Geometry on the Resonance Frequency of Helmholtz Resonators,” Journal of Sound and Vibration, 178, pp. 337–348 (1994).Google Scholar
6. Dickey, N. S. and Selamet, A., “Helmholtz Resonators: One-dimensional Limit for Small Cavity Length-to-diameter Ratios,” Journal of Sound and Vibration, 195, pp. 512–517 (1996).Google Scholar
7. Tang, S. K., “On Helmholtz Resonators with Tapered Necks,” Journal of Sound and Vibration, 279, pp. 1085–1096 (2005).Google Scholar
8. Chaudhari, M., Verma, G. and Puranik, B., “Frequency Response of a Synthetic Jet Cavity,” Experimental Thermal and Fluid Science, 33, pp. 439–448 (2009)Google Scholar
9. Krishnan, G. and Mohseni, K., “An Experimental and Analytical Investigation of Rectangular Synthetic Jets,” Journal of Fluids Engineering, 131, pp. 121101-1–11 (2009).Google Scholar
10. Kim, S. H. and Kim, C. G., “Separation Control on NACA23012 Using Synthetic Jet,” Aerospace Science and Technology, 13, pp 172–182 (2009).Google Scholar
11. Amir, M. and Kontis, K., “Application of Piezoelectric Actuators at Subsonic Speeds,” Journal of Aircraft, 45, pp. 1419–1430 (2008).Google Scholar
12. Farnsworth, J. A. N., Vaccaro, J. C. and Amitay, M., “Active Flow Control at Low Angles of Attack: Stingray Unmanned Aerial Vehicle,” AIAA Journal, 46, pp. 2530–2544 (2008)Google Scholar
13. Ciuryla, M., Liu, Y., Famsworth, J., Kwan, C. and Amitay, M., “Flight Control Using Synthetic Jets on a Cessna 182 Model,” Journal of Aircraft, 44, pp. 643–653 (2007).Google Scholar
14. Chiders, D. G., Probability and Random Process, McGraw-Hill, New York, pp. 290–291 (1997).Google Scholar
15. Watson, M., Jaworski, A. J. and Wood, N. J., “Contribution to the Understanding of Flow Interactions Between Multiple Synthetic Jets,” AIAA Journal, 41, pp. 747–749 (2008).CrossRefGoogle Scholar