Research on high attack angle stall and spin characteristics with flight test of a general electric aircraft
When the aircraft is flying at high angle of attack, the local separation of the air flow on the surface of the aircraft, the linear change of aerodynamic force is destroyed, and the maneuverability and stability are reduced to varying degrees, resulting in the aircraft stalling or entering the spin...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
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/jnwpu2021393p650/jnwpu2021393p650.html |