Influences of distributed propulsion system parameters on aerodynamic characteristics of a BLI-BWB UAV
Focusing on the aerodynamic characteristics of the blended wing body (BWB) aircraft with boundary layer ingestion(BLI) distributed propulsion system; the influences of propulsion system parameters under the condition of cruise and takeoff are studied. Firstly, based on the momentum source method (MS...
| Format: | Article |
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| Language: | zho |
| Published: |
EDP Sciences
2021-02-01
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| Series: | Xibei Gongye Daxue Xuebao |
| Subjects: | |
| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/01/jnwpu2021391p17/jnwpu2021391p17.html |