Add to ORKGA cyclocopter propelled by the cycloidal blade system, which can be described as a horizontal rotary wing, is a new concept of VTOL vehicle. In this paper, structural design and analysis are carried out for the aerodynamically optimized cyclocopter rotor system. Design variables such as stacking sequence (ply angles), number of plies and locations of spars of composite blade are determined through MSC/NASTRAN, RSM and some other optimizing processes. The maximum stress obtained by static analysis of each parts of the rotor is within the failure criteria. The rotor system is designed for the purpose of avoiding possible dynamic instabilities by inconsistency between frequencies of rotor rotation and some low natural frequencies of rotor. Als...
In the helicopter, the main rotor blade is mostly influenced by the aerodynamic forces and centrifug...
Purpose: The purpose of this paper is to define an optimal pitching profile for the blades of a cycl...
Most military grade micro air vehicles do not have the ability to hover. In order to try to create ...
A cyclocopter propelled by the cycloidal blade system is a new concept of VTOL vehicle which has exc...
Cycloidal rotors consist of an arrangement of blades that rotate and pitch about a central drum. The...
The cycloidal propeller, which can be described as a horizontal rotary wing, offers powerful thrust ...
Purpose-Few modeling approaches exist for cycloidal rotors because they are a prototypal technology....
The cycloidal blades system is a thrust propulsion system that consists of several blades rotating a...
A cyclorotor (also known as a cyclocopter or cyclogiro) is a rotating-wing system where the span of ...
This paper describes the aeroelastic model to predict the blade loads and the average thrust of a mi...
The aeroelasticity of a cycloidal rotor in forward flight is investigated using an analytical and a ...
In this study, not only the principle of the thrust control for the VTOL UAV cyclocopter with cycloi...
In this work, four key design parameters of cycloidal rotors, namely the airfoil section, number of ...
In the helicopter, the main rotor blade is mostly influenced by the aerodynamic forces and centrifug...
Purpose: The purpose of this paper is to define an optimal pitching profile for the blades of a cycl...
Most military grade micro air vehicles do not have the ability to hover. In order to try to create ...
A cyclocopter propelled by the cycloidal blade system is a new concept of VTOL vehicle which has exc...
Cycloidal rotors consist of an arrangement of blades that rotate and pitch about a central drum. The...
The cycloidal propeller, which can be described as a horizontal rotary wing, offers powerful thrust ...
Purpose-Few modeling approaches exist for cycloidal rotors because they are a prototypal technology....
The cycloidal blades system is a thrust propulsion system that consists of several blades rotating a...
A cyclorotor (also known as a cyclocopter or cyclogiro) is a rotating-wing system where the span of ...
This paper describes the aeroelastic model to predict the blade loads and the average thrust of a mi...
The aeroelasticity of a cycloidal rotor in forward flight is investigated using an analytical and a ...
In this study, not only the principle of the thrust control for the VTOL UAV cyclocopter with cycloi...
In this work, four key design parameters of cycloidal rotors, namely the airfoil section, number of ...
In the helicopter, the main rotor blade is mostly influenced by the aerodynamic forces and centrifug...
Purpose: The purpose of this paper is to define an optimal pitching profile for the blades of a cycl...
Most military grade micro air vehicles do not have the ability to hover. In order to try to create ...