Investigation of flow over oscillating NACA 4421airfoils in tandem configuration at low Reynolds number
The present study is on the experimental investigation of the flow over oscillating NACA4421 airfoils in various tandem configurations at low Reynolds number of 8.6 x 103. Force and two dimensional particle image velocimetry (PIV) measurements were carried out in the NTU closed loop water tunnel wit...
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| Format: | Thesis |
| Language: | English |
| Published: |
2019
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| Online Access: | https://hdl.handle.net/10356/88856 http://hdl.handle.net/10220/47648 |