Title :
A computing model of PZT-driven synthetic jet actuator
Author :
Luo, Zhen-bing ; Xia, Zhi-xun ; Wang, Lin
Author_Institution :
Coll. of Aerosp. & Mater. Eng., Nat. Univ. of Defense Technol., Changsha, China
Abstract :
Synthetic jet actuators (SJAs) with the piezoelectric (PZT) vibrator in clamped and simply supported edge conditions are investigated. The vibrating characteristics of the PZT vibrator are investigated, and a delay phase of PZT vibrator is put forward. According to the vibrating characters of the PZT vibrator, the LUO-XIA model, a computing model of the SJA is established, in which the delay phase angle, time function, displacement distribution, and supported conditions of PZT vibrator are take into account. Then the synthetic jet flow-field is simulated, and results are compared with experiments. Results show the LUO-XIA model is correct and considerate.
Keywords :
jets; lead compounds; piezoelectric actuators; vibration measurement; LUO-XIA model; PZT; PZT-driven synthetic jet actuator; computing model; delay phase angle; displacement distribution; piezoelectric vibrator; time function; vibrating characteristics; Aerospace engineering; Aerospace materials; Computational modeling; Delay effects; Distributed computing; Educational institutions; Piezoelectric actuators; Piezoelectric materials; System testing; Voltage; LUO-XIA model; Synthetic jet actuator; computing model; piezoelectric vibrator;
Conference_Titel :
Piezoelectricity, Acoustic Waves, and Device Applications (SPAWDA) and 2009 China Symposium on Frequency Control Technology, Joint Conference of the 2009 Symposium on
Conference_Location :
Wuhan
Print_ISBN :
978-1-4244-4950-7
DOI :
10.1109/SPAWDA.2009.5428924
