STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
Guardado en:
| Autor Corporativo: | |
|---|---|
| Otros Autores: | , |
| Formato: | Libro |
| Lenguaje: | inglés |
| Publicado: |
Dhaka :
ME DEPT. MIST,
c2014.
|
| Materias: | |
| Etiquetas: |
Sin Etiquetas, Sea el primero en etiquetar este registro!
|
Ejemplares similares: 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 /