An experimental investigation of the effects of dynamic motions on a delta wing
The final year project involves the investigation on the vortex breakdown phenomenon associated with dynamic pitching and dynamic rolling delta wing. Experimental investigation was performed on a 70o sweep delta wing with aspect ratio 1.46 at a Reynolds number of 15750in a water tunnel of Nanyang Te...
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| Format: | Final Year Project |
| Language: | English |
| Published: |
2012
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| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/50468 |
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| Institution: | Nanyang Technological University |
| Language: | English |
| Summary: | The final year project involves the investigation on the vortex breakdown phenomenon associated with dynamic pitching and dynamic rolling delta wing. Experimental investigation was performed on a 70o sweep delta wing with aspect ratio 1.46 at a Reynolds number of 15750in a water tunnel of Nanyang Technological University. The vortex breakdown location of delta wing under steady state and dynamic motion was visualized using dye injection. |
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