Development Of Design Of Aerofoil Shaped Fuselage And CFD Investigation Of Its Aerodynamic Characteristics
This paper explains about the computational design procedure for designing of an Unmanned Air Vehicles (UAV) having “Aerofoil Shaped Fuselage”. It also explains and analyses of the aerodynamic characteristics of an “Aerofoil Shaped Fuselage”. This model could be used for designing of the future UAV...
Spremljeno u:
| Glavni autori: | , , , |
|---|---|
| Format: | Članak |
| Jezik: | engleski |
| Izdano: |
R&D Wing, MIST
2015
|
| Teme: | |
| Online pristup: | http://hdl.handle.net/123456789/221 |
| Oznake: |
Bez oznaka, Budi prvi tko označuje ovaj zapis!
|
Slični predmeti: Development Of Design Of Aerofoil Shaped Fuselage And CFD Investigation Of Its Aerodynamic Characteristics
- AN EXPERIMENTAL INVESTIGATION OF WIND LOAD ON TALL BUILDINGS WITH HEXAGONAL CROSS-SECTION
- STRUCTURAL DESIGN, ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE
- STUDY OF AERODYNAMICS OF A CRICKET BALL
- STUDY OF AERODYNAMICS OF A CRICKET BALL
- PERFORMANCE ANALYSIS OF WIND TURBINES WITH TIP VANES
- Design Aid For Continuous Beams