Add to ORKGIn this paper an acousto-structural control approach has been developed for the limitation of interior noise an a turbopro airctaft. The approach involve the use of piezoelectric actuators bondend on the primaruy structure of the aircraft and acoustic sensors distributed inside the acoustic cavity. An optimization process of the relative numbe and the control parameters have been optimized by the use of Artificial Neural Network algorithms, specifically developed for the application
Active noise control is the art of reducing a primary unwanted sound field by interference with an a...
One of the main objectives of efficient aircraft design, alongside safety and fuel consumption, is i...
Noise reduction in the transmission path of aircraft panels is a crucial step of enhanced designs f...
In this paper an acousto-structural control approach has been developed for the limitation of interi...
The possibility of guaranteeing significant fuel savings has undoubtedly contributed to the diffusio...
During the last five years, the Dept. of Aeronautical Engineering of the University of Naples, has c...
This paper describes preliminary laboratory experiments conducted on a turboprop aircraft fuselage t...
This paper describes preliminary laboratory experiments conducted on a turboprop aircraft fuselage t...
International audienceThis paper reports on the design and optimization of different types of piezoe...
"\"An integrated spectral-integral formulation is applied for prediction and active control of. the ...
A study of the Active Structural Acoustic Control (ASAC) of a full scale deHavilland Dash-8 series 1...
This paper presents the activities developed by the authors within the first year of the research pr...
Cabin noise in turboprop aircraft causes passenger discomfort, airframe fatigue, and employee schedu...
This paper presents the activities developed by the authors within the first year of the research pr...
This paper deals with the abatement of the tonal noise inside the fuselage of a mid-range tiltrotor ...
Active noise control is the art of reducing a primary unwanted sound field by interference with an a...
One of the main objectives of efficient aircraft design, alongside safety and fuel consumption, is i...
Noise reduction in the transmission path of aircraft panels is a crucial step of enhanced designs f...
In this paper an acousto-structural control approach has been developed for the limitation of interi...
The possibility of guaranteeing significant fuel savings has undoubtedly contributed to the diffusio...
During the last five years, the Dept. of Aeronautical Engineering of the University of Naples, has c...
This paper describes preliminary laboratory experiments conducted on a turboprop aircraft fuselage t...
This paper describes preliminary laboratory experiments conducted on a turboprop aircraft fuselage t...
International audienceThis paper reports on the design and optimization of different types of piezoe...
"\"An integrated spectral-integral formulation is applied for prediction and active control of. the ...
A study of the Active Structural Acoustic Control (ASAC) of a full scale deHavilland Dash-8 series 1...
This paper presents the activities developed by the authors within the first year of the research pr...
Cabin noise in turboprop aircraft causes passenger discomfort, airframe fatigue, and employee schedu...
This paper presents the activities developed by the authors within the first year of the research pr...
This paper deals with the abatement of the tonal noise inside the fuselage of a mid-range tiltrotor ...
Active noise control is the art of reducing a primary unwanted sound field by interference with an a...
One of the main objectives of efficient aircraft design, alongside safety and fuel consumption, is i...
Noise reduction in the transmission path of aircraft panels is a crucial step of enhanced designs f...