STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /
Saved in:
| Corporate Author: | |
|---|---|
| Other Authors: | , |
| Format: | Book |
| Language: | English |
| Published: |
Dhaka :
ME DEPT. MIST,
c2014.
|
| Subjects: | |
| Tags: |
No Tags, Be the first to tag this record!
|
Similar Items: 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 /