Landing gear design in an automated design environment
Automation of the design process of aircraft landing gear. Requirements for placement of the chassis on the aircraft: takeoff, landing, stability, handling and stability when taxiing etc. Empirical type models, motion and forces at the contact point.
| Рубрика | Транспорт |
| Предмет | Transport |
| Вид | магистерская работа |
| Язык | английский |
| Прислал(а) | N.C. Heerens |
| Дата добавления | 30.11.2016 |
| Размер файла | 6,1 M |
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