Preliminary Determination of Propeller Aerodynamic Characteristics for Small Aeroplanes
Conducting a preliminary determination of the propeller thrust and power coefficients depending on the predetermined relationship with the help of representative geometrical parameters of the blade at a certain radius. Evaluation of nonlinear influence.
| Рубрика | Физика и энергетика |
| Предмет | Аerodynamics |
| Вид | статья |
| Язык | английский |
| Прислал(а) | Анна |
| Дата добавления | 08.10.2013 |
| Размер файла | 187,3 K |
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