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.

Detalles Bibliográficos
Autor principal: Villarreal Valderrama, José Francisco
Formato: Tesis
Lenguaje:English
Publicado: 2019
Materias:
Acceso en línea:http://eprints.uanl.mx/18836/1/1080252232.pdf