—The aerospace industry deals from the beginning with structures with special requirements as extreme lightweight and withstanding to a big number of load cases. Aerodynamics constraints lead to supplementary restrictions, the results being the complex shape to sustain the fuselage, the rotor blades or the wings skin. This paper presents a static structural analysis of the main rotor blade for the light helicopter. To simulate the mechanical behavior of the blade, a finite elements method was used. A case of hovering flight mode was considered
A framework is described and demonstrated for CFD analysis of helicopter rotors in hover and forward...
Structural strength is just as important as any other measures for a performance vehicle - let it be...
The present investigation concerns itself almost completely with the derivation and solution of the ...
In the helicopter, the main rotor blade is mostly influenced by the aerodynamic forces and centrifug...
In this paper, helicopter rotor blades are analysed in hover using computational fluid dynamics (CFD...
In this paper, helicopter rotor blades are analysed in hover using computational fluid dynamics (CFD...
A new method used to analyze the aeroelastic stability of a helicopter hingeless blade in hovering h...
Results of calculation of the helicopter main rotor loads and deformations of rotor blades are prese...
An aeroelastic analysis based on finite elements in space and time is used to model the helicopter r...
An aeroelastic analysis based on finite elements in space and time is used to model the helicopter r...
Results of simulation of main rotor blade loads and deformations, which can be generated during boun...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
In this work, the homemade helicopter aerodynamics is analyzed. The helicopter model is the Sikorsky...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...
A framework is described and demonstrated for CFD analysis of helicopter rotors in hover and forward...
Structural strength is just as important as any other measures for a performance vehicle - let it be...
The present investigation concerns itself almost completely with the derivation and solution of the ...
In the helicopter, the main rotor blade is mostly influenced by the aerodynamic forces and centrifug...
In this paper, helicopter rotor blades are analysed in hover using computational fluid dynamics (CFD...
In this paper, helicopter rotor blades are analysed in hover using computational fluid dynamics (CFD...
A new method used to analyze the aeroelastic stability of a helicopter hingeless blade in hovering h...
Results of calculation of the helicopter main rotor loads and deformations of rotor blades are prese...
An aeroelastic analysis based on finite elements in space and time is used to model the helicopter r...
An aeroelastic analysis based on finite elements in space and time is used to model the helicopter r...
Results of simulation of main rotor blade loads and deformations, which can be generated during boun...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
In this work, the homemade helicopter aerodynamics is analyzed. The helicopter model is the Sikorsky...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...
Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to...
A framework is described and demonstrated for CFD analysis of helicopter rotors in hover and forward...
Structural strength is just as important as any other measures for a performance vehicle - let it be...
The present investigation concerns itself almost completely with the derivation and solution of the ...