Aerodynamic interactions analysis of propeller configurations and spatial parameters on a twin-boom unmanned aerial vehicle
To overcome the technical bottleneck in aircraft design where aerodynamic and propulsion systems are treated separately, an integrated actuator disk model (ADM) simulation platform based on blade element momentum theory (BEMT) was developed, enabling efficient evaluation of propeller–aircraft aerody...
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| Principais autores: | , , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado em: |
Taylor & Francis Group
2026-12-01
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| coleção: | Engineering Applications of Computational Fluid Mechanics |
| Assuntos: | |
| Acesso em linha: | https://www.tandfonline.com/doi/10.1080/19942060.2026.2678120 |
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