STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
Uloženo v:
| Korporativní autor: | |
|---|---|
| Další autoři: | , |
| Médium: | Kniha |
| Jazyk: | angličtina |
| Vydáno: |
Dhaka :
ME DEPT. MIST,
c2014.
|
| Témata: | |
| Tagy: |
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!
|
Podobné jednotky: STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
- STRUCTURAL DESIGN, ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE
- INVESTIGATION OF THE EFFECT OF DIFFERENT AIRFOIL SHAPED FUSELAGE ON THE PERFORMANCE OF AN UNMANNED AIR VEHICLE /
- EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF THE CHARACTERISTICS OF NACA 4412 AEROFOIL USING DIFFERENT SHAPES /
- Development Of Design Of Aerofoil Shaped Fuselage And CFD Investigation Of Its Aerodynamic Characteristics
- DESIGN AND CONSTRUCTION OF FLAPPING WING AERIAL VEHICLE (FWAV) /
- DESIGN AND FABRICATION OF THE FUSELAGE OF A RADIO CONTROLLED AERIAL VEHICLE /