Numerical and analytical modeling of the propulsive wing and fuselage of an air taxi
The problem of creating propulsive airfoils is considered. Such airfoils have a slit through which the boundary layer is sucked out. Located just behind this gap, a specially profiled section of the airfoil creates a propulsive thrust. The thrust is created due to an abrupt change in the pressure pr...
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| Principais autores: | , , |
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| Format: | Artigo |
| Sprog: | Inglês |
| Udgivet: |
ITMO University
2024-12-01
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| Serier: | Научно-технический вестник информационных технологий, механики и оптики |
| Fag: | |
| Online adgang: | https://ntv.elpub.ru/jour/article/view/348 |
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