Research on the forward flight performance of rotor based on variable-droop leading edge
Aiming at the dynamic stall phenomenon of the retreating side of the rotor in forward flight, the existing flow control method of dynamic leading edge droop was applied to the flow control of forward-flying rotor at three-dimensional scale. A numerical simulation method based on variable droop leadi...
| Format: | Article |
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| Language: | zho |
| Published: |
The Northwestern Polytechnical University
2021-06-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/03/jnwpu2021393p668/jnwpu2021393p668.html |