STRUCTURAL DESIGN, ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE
This project and dissertation is a significant outcome of supreme guidance and concentrated team effort. We respectfully acknowledge the cordial help of individuals who played distinct role for the successful accomplishment of the project. We offer our deepest gratitude to our supervisor Wg Cdr Dr G...
Збережено в:
| Автори: | , , |
|---|---|
| Формат: | Дисертація |
| Мова: | Англійська |
| Опубліковано: |
Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST)
2016
|
| Предмети: | |
| Онлайн доступ: | http://hdl.handle.net/123456789/245 |
| Теги: |
Немає тегів, Будьте першим, хто поставить тег для цього запису!
|
Search Result 1