Experimental and Computational Analysis of Single Crystal Piezoelectrical Driven Synthetic Jet Actuator
TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) , Madrid, İspanya, 1 - 04 Temmuz 2019, ss.1-10, (Tam Metin Bildiri)
- Yayın Türü: Bildiri / Tam Metin Bildiri
- Doi Numarası: 10.13009/eucass2019-380
- Basıldığı Şehir: Madrid
- Basıldığı Ülke: İspanya
- Sayfa Sayıları: ss.1-10
- Orta Doğu Teknik Üniversitesi Kuzey Kıbrıs Kampüsü Adresli: Hayır
Özet
This study aims to examine the velocity and efficiency improvement of a synthetic jet actuator by utilizing a single-crystal piezoelectric disc. Laser vibrometer and hot-wire anemometry were used in the experiments to measure diaphragm displacement and output velocity, respectively. Experiments achieved a peak electro-fluidic power conversion efficiency of 43% with a peak output jet velocity of 114 m/s. A multi-physics computational simulation was developed to reproduce the experimental results. The simulation results showed an acceptable match with experimental data. Peak displacement and peak output jet velocity matched with 5% and 3% with experimental data, respectively.