Investigation of Slotted Tip Parameters on the Aerodynamic Characteristic of Helicopter Rotor
Numerical simulations are conducted to investigate the effect of helicopter rotor tip vortex alleviation using a slotted tip, and effects of parameters involving location, number, aperture of the slot on tip vortex structure and aerodynamic performance are analyzed in detail. The flow field of hover...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
2018-08-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/pdf/2018/04/jnwpu2018364p778.pdf |