AERODYNAMIC PERFORMANCE ANALYSIS AND PROPULSION SYSTEM DESIGN OF AN UNMANNED AERIAL VEHICLE USING NACA 4415 PROFILE / LT Tarik, LT Nabila, Nayeema parvin .
Сохранить в:
| Главный автор: | |
|---|---|
| Соавтор: | |
| Другие авторы: | |
| Формат: | |
| Язык: | английский |
| Опубликовано: |
Dhaka :
ME DEPT MIST ,
c 2014 .
|
| Предметы: | |
| Метки: |
Нет меток, Требуется 1-ая метка записи!
|
Схожие документы: AERODYNAMIC PERFORMANCE ANALYSIS AND PROPULSION SYSTEM DESIGN OF AN UNMANNED AERIAL VEHICLE USING NACA 4415 PROFILE /
- ''DESIGN DEVELOPMENT AND PERFORMANCE ANALYSIS OF THE PROPULSION SYSTEM OF A SHORT RANGE UNMANNED AERIAL VEHICLE''
- "DESIGN FABRICATION,DEVELOPMENT AND PERFORMANCE ANALYSIS OF THE PROPULSION SYSTEM OF A SMALL SURVEILLANCE UNMANNED AERIAL VEHICLE" /
- A COMPARATIVE STUDY OF AERODYNAMIC CHARACTERISTICS OF NACA 0015 AND NACA 4415 AIRFOILS AT VARIOUS REYNOLDS NUMBER /
- DESIGN OF A FIXED WING JET PROPULSION POWERED UNMANNED AERIAL VEHICLE (UAV) TARGET DRONE /
- DESIGN AND FABRICATION OF AN UNMANNED AERIAL VEHICLE EATABLE OF DELIVERING MISSION PAYLOAD /
- "DESIGN,FABRICATION AND DEVELOPMENT OF AN UNMANNED AERIAL VEHICLE CAPABLE OF DELIVERING MISSION PAYLOAD"