The continuous progress made in computer science and mathematics has allowed simulation to take a growing place in modern engineering. It is today a strategic stake for research as well as industry. Indeed, it allows a better apprehension of many fields of study, going from physics to biology through economics to mention a few. In aeronautics, simulation might come before production to avoid any fatal error in aircraft safety, or after production as a maintenance tool. It has many purposes, but it is always a compromise between the degree of subtlety of modeling and the calculation capacity of a computer. This paper presents and compares two simulation codes in rotorcraft engineering. Both are used professionally by private companies. The m...
Some of the more challenging aspects of modelling the mechanical dynamics of rotorcraft systems are ...
For the validation of rotor blade designs a multibody system model of a helicopter with main rotor -...
The work carried out in this thesis consists in the development and testing of two helicopter mathem...
The continuous progress made in computer science and mathematics has allowed simulation to take a gr...
The scope and usefulness of a flight simulator goes well beyond its pilot training capabilities; in...
Various features of the computer codes used in the helicopter industry and by government agencies fo...
This paper describes the design and manufacturing of the AgustaWestland flight mechanics simulator f...
Helicopters have been valuable vehicles ever since their invention. Their capabilities for axial fli...
The simulation of the helicopter motion is a central component in e.g. flight control design, handli...
The simulation of the helicopter motion is a central component in flight control design, handling qu...
The purpose of this project is to numerically develop a code that computes the different forces on t...
The development of rotary aircraft has progressed by leap and bounds since the early 20th century. P...
Helicopter flight dynamic, rotor aerodynamic and dynamic analyses activities have been a great dispu...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
Abstract — This paper considers modelling and simulation study of a helicopter system – UH-60 Black ...
Some of the more challenging aspects of modelling the mechanical dynamics of rotorcraft systems are ...
For the validation of rotor blade designs a multibody system model of a helicopter with main rotor -...
The work carried out in this thesis consists in the development and testing of two helicopter mathem...
The continuous progress made in computer science and mathematics has allowed simulation to take a gr...
The scope and usefulness of a flight simulator goes well beyond its pilot training capabilities; in...
Various features of the computer codes used in the helicopter industry and by government agencies fo...
This paper describes the design and manufacturing of the AgustaWestland flight mechanics simulator f...
Helicopters have been valuable vehicles ever since their invention. Their capabilities for axial fli...
The simulation of the helicopter motion is a central component in e.g. flight control design, handli...
The simulation of the helicopter motion is a central component in flight control design, handling qu...
The purpose of this project is to numerically develop a code that computes the different forces on t...
The development of rotary aircraft has progressed by leap and bounds since the early 20th century. P...
Helicopter flight dynamic, rotor aerodynamic and dynamic analyses activities have been a great dispu...
The paper deals with the assessment of the reliability of simplified rotorcraft models in the evalua...
Abstract — This paper considers modelling and simulation study of a helicopter system – UH-60 Black ...
Some of the more challenging aspects of modelling the mechanical dynamics of rotorcraft systems are ...
For the validation of rotor blade designs a multibody system model of a helicopter with main rotor -...
The work carried out in this thesis consists in the development and testing of two helicopter mathem...