کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
5008173 | 1461834 | 2017 | 12 صفحه PDF | دانلود رایگان |
- Changes to synthetic jet actuator geometry are explored to reduce actuator noise.
- Double-chamber actuators reduce noise through dipole/anti-phase effect.
- Lobed-orifice actuators reduce noise through intensified mixing of the jet flow.
- Demonstrable levels of noise reduction are achieved without significantly reducing jet velocity.
This work details an experimental investigation aimed at reducing the noise output of piezoelectrical-driven synthetic jet actuators while minimising peak jet velocity reduction. The study considers double-chamber actuator for anti-phase noise suppression and lobed orifice as a method to enhance jet turbulent mixing to suppress jet noise. The study involved the design, manufacture and bench test of interchangeable actuator hardware. Hot-wire anemometry and microphone recordings were employed to acquire velocity and sound pressure level measurements respectively across a range of excitation frequencies for a fixed diaphragm clamping and input voltage. The data analysis indicated a 26% noise reduction (16Â dB) from operating a single-chamber, round orifice actuator to a double-chamber, lobed orifice one at the synthetic jet resonant frequency. Results also showed there was a small reduction in peak jet velocity of 7% (â¼3Â m/s) between these two cases based on orifices of the same discharge area. The electrical-to-fluidic power conversion efficiency of the double-chamber actuator was found to be 15% for both orifice types at the resonant frequency; approximately double the efficiency of a single-chamber actuator.
Journal: Sensors and Actuators A: Physical - Volume 266, 15 October 2017, Pages 273-284