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...
Sábháilte in:
| Príomhchruthaitheoirí: | , , |
|---|---|
| Formáid: | Tráchtas |
| Teanga: | Béarla |
| Foilsithe / Cruthaithe: |
Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST)
2016
|
| Ábhair: | |
| Rochtain ar líne: | http://hdl.handle.net/123456789/245 |
| Clibeanna: |
Níl clibeanna ann, Bí ar an gcéad duine le clib a chur leis an taifead seo!
|
Míreanna comhchosúla: STRUCTURAL DESIGN, ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE
- Development Of Design Of Aerofoil Shaped Fuselage And CFD Investigation Of Its Aerodynamic Characteristics
- STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
- Mechanics of flight /
- Mechanics of Flight /
- STUDY OF THE INFLUENCE OF LEADING EDGE ROTATING CYLINDER ON THE PERFORMANCE OF A SYMMETRIC AEROFOIL
- Mechanics of flight /