International audienceThis paper introduces recent developments in the computation of rotorcraft noise footprint, implemented in an Airbus Helicopters' internal software. The paper presents the main ingredients that have led to enhance the efficiency and accuracy of such noise footprint computation. This includes taking into account both the particularities of turns in noise emission and the influence of the wind on noise propagation. Furthermore, the software is able to assess a real traffic environmental impact, since computations are done within a realistic 3D simulation environment, taking into account both the curvature of the Earth and the topography of the ground. A variety of noise annoyance indicators can be computed thanks to the ...
The main aim of this study is to provide a multi-disciplinary optimization and track environment to ...
Based on the acoustic mapping, a prediction model for the ground noise radiated from an in-flight he...
Noise emission is a limiting factor for helicopter operations. Additional to new helicopter designs,...
International audienceAviation is heading towards more sustainability. In this context, this paper p...
"A software suite is presented that aims to optimize rotorcraft trajectories with respect to the env...
This paper presents a numerical technique for the noise ground footprint prediction for given helico...
This paper discusses the development of a software suite that aims to optimize helicopter trajectori...
As a first step towards noise abatement flight procedure design, this report presents a numerical te...
Next generation commercial air transportation will likely see an increased use of rotorcraft, includ...
This paper presents a computational tool to predict the ground noise footprint of a complete helicop...
As a first step towards noise abatement flight procedure design, this paper presents techniques for ...
This paper describes the implementation of the DLR SELENE computation chain, able to predict the noi...
This paper investigates different techniques for the evaluation of the acoustic disturbance emitted ...
A study is presented that aims to synthesize rotorcraft-specific Simultaneous Non-Interfering approa...
As a first step towards noise abatement flight procedure design, this paper presents techniques for ...
The main aim of this study is to provide a multi-disciplinary optimization and track environment to ...
Based on the acoustic mapping, a prediction model for the ground noise radiated from an in-flight he...
Noise emission is a limiting factor for helicopter operations. Additional to new helicopter designs,...
International audienceAviation is heading towards more sustainability. In this context, this paper p...
"A software suite is presented that aims to optimize rotorcraft trajectories with respect to the env...
This paper presents a numerical technique for the noise ground footprint prediction for given helico...
This paper discusses the development of a software suite that aims to optimize helicopter trajectori...
As a first step towards noise abatement flight procedure design, this report presents a numerical te...
Next generation commercial air transportation will likely see an increased use of rotorcraft, includ...
This paper presents a computational tool to predict the ground noise footprint of a complete helicop...
As a first step towards noise abatement flight procedure design, this paper presents techniques for ...
This paper describes the implementation of the DLR SELENE computation chain, able to predict the noi...
This paper investigates different techniques for the evaluation of the acoustic disturbance emitted ...
A study is presented that aims to synthesize rotorcraft-specific Simultaneous Non-Interfering approa...
As a first step towards noise abatement flight procedure design, this paper presents techniques for ...
The main aim of this study is to provide a multi-disciplinary optimization and track environment to ...
Based on the acoustic mapping, a prediction model for the ground noise radiated from an in-flight he...
Noise emission is a limiting factor for helicopter operations. Additional to new helicopter designs,...