Add to ORKGTilt-wing and tilt-rotor unmanned aerial vehicles (UAVs) represents promising direction for the future development. This paper presents the method for the preliminary design optimization of the propeller for such vehicle. It should be capable to generate high thrust in both forward flight and hover modes. This brings design challenges for the propeller aerodynamic design. All considered variants have same number of blades, engine power, airfoils and diameter. Thrust in forward cruise speed 30 m/s and in hover is computed and compared by the means of Pareto diagram. Choose of the optimal RPM is based on the computation results
This paper describes the design of a turboshaft engine for a tiltwing air taxi application. In this ...
In this study, the design and analysis of hovering controller of an UAV which is capable of doing ve...
Small-unmanned aerial vehicle propellers usually have a low figure of merit due to operating in the ...
Tilt-wing and tilt-rotor unmanned aerial vehicles (UAVs) represents promising direction for the futu...
Unmanned Aerial Vehicles (UAVs) are used on a wide range of missions depending on the situation and ...
This project research presents the conceptual design of a Tilt-rotor Unmanned Aerial Vehicle (UAV), ...
The aerodynamic shape design of a proprotor for a tiltrotor aircraft is a very complex and demanding...
This paper presents a methodology to design the optimum proprotor for tilt-body microair-vehicles (T...
Purpose - The purpose of this paper is to present the aerodynamic blade design of a tiltwing aircraf...
This study introduces the simulation of a tri-rotor contra-rotating propeller for thrust force and h...
Nowadays, civil UAV industry market grows rapidly. This expansion is followed by the new requirement...
Osnovne uloge bespilotnih letelica podrazumevaju: osmatranje, nadzor, prenos robe, daljinsko očitava...
The popularity of Unmanned Aerial Vehicles (UAV) has been increasing rapidly over the past few year...
Unmanned aerial vehicles are increasingly deployed in various applications such as surveillance, map...
A tilt rotor is an aircraft of a special kind, which possesses the characteristics of a helicopter a...
This paper describes the design of a turboshaft engine for a tiltwing air taxi application. In this ...
In this study, the design and analysis of hovering controller of an UAV which is capable of doing ve...
Small-unmanned aerial vehicle propellers usually have a low figure of merit due to operating in the ...
Tilt-wing and tilt-rotor unmanned aerial vehicles (UAVs) represents promising direction for the futu...
Unmanned Aerial Vehicles (UAVs) are used on a wide range of missions depending on the situation and ...
This project research presents the conceptual design of a Tilt-rotor Unmanned Aerial Vehicle (UAV), ...
The aerodynamic shape design of a proprotor for a tiltrotor aircraft is a very complex and demanding...
This paper presents a methodology to design the optimum proprotor for tilt-body microair-vehicles (T...
Purpose - The purpose of this paper is to present the aerodynamic blade design of a tiltwing aircraf...
This study introduces the simulation of a tri-rotor contra-rotating propeller for thrust force and h...
Nowadays, civil UAV industry market grows rapidly. This expansion is followed by the new requirement...
Osnovne uloge bespilotnih letelica podrazumevaju: osmatranje, nadzor, prenos robe, daljinsko očitava...
The popularity of Unmanned Aerial Vehicles (UAV) has been increasing rapidly over the past few year...
Unmanned aerial vehicles are increasingly deployed in various applications such as surveillance, map...
A tilt rotor is an aircraft of a special kind, which possesses the characteristics of a helicopter a...
This paper describes the design of a turboshaft engine for a tiltwing air taxi application. In this ...
In this study, the design and analysis of hovering controller of an UAV which is capable of doing ve...
Small-unmanned aerial vehicle propellers usually have a low figure of merit due to operating in the ...