Method of first-approximation calculation of take-off weight of a light aircraft with a hybrid propulsion system
The article discusses a method for calculating, as a first approximation, the take-off weight of a light aircraft with a hybrid power plant based on piston and electric engines. A brief overview of organizations dealing with hybrid power plants is given. The influence of the degree of hybridization...
| Published in: | Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение |
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| Main Authors: | , , |
| Format: | Article |
| Language: | English |
| Published: |
Samara National Research University
2024-07-01
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| Subjects: | |
| Online Access: | https://journals.ssau.ru/vestnik/article/viewFile/27656/10659 |
