Analysis and modeling of micro turbojets: a comprehensive model based on multiphysics principles.
The Development of accurate models to represent turbojet performance is presented as a tool to meet the growing need for reliable unmanned aerial vehicle propulsion systems.
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| Formato: | Tesis |
| Lenguaje: | inglés |
| Publicado: |
2019
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| Acceso en línea: | http://eprints.uanl.mx/18836/1/1080252232.pdf |