In this study, the concept of a Zero Mass Flow Liner is evaluated. The concept enables impedance control by the induction of periodic bias flow through the perforated facing sheet of the liner. The periodic bias flow is generated by a secondary high amplitude acoustic actuation. By means of the periodic bias flow, the liner can be tuned to different operating points in a given range of grazing flow velocities. The equivalent fluid impedance model for perforated plates is modified to account for the effects of periodic bias flow and grazing flow. An optimization routine, based on a genetic algorithm, is implemented. The method is applicable to any liner concept and uses the impedance of the lined surface as boundary condition in a numerical ...
Interest in characterization of the aerodynamic drag of acoustic liners has increased in the past se...
Interest in the characterization of the aerodynamic drag performance of acoustic liners has increase...
Over the past several years, the NASA Langley Liner Physics Team has worked to develop methods capab...
In this study, the concept of a zero mass flow liner is evaluated. The concept enables impedance con...
The Zero Mass Flow Liner is able to convert a perforated liner with minimal damping qualities into a...
Modern aero-engines require due to their architecture an enhanced damping performance of passive, ac...
This thesis is motivated by the need for noise control in aircraft engine with orifices and perforat...
Because communities are impacted by steady increases in aircraft traffic, aircraft noise continues t...
The aerodynamic drag of acoustic liners has become a significant topic in the design of such for air...
The study of normal impedance of perforated plate acoustic liners including the effect of bias flow ...
In the field of noise reduction of aero-engines passive acoustic silencers, so-called liners still s...
Modern, low-emission aero-engine concepts, such as, for instance, Ultrahigh-Bypass Ratio (UHBR) desi...
Through this project, the effectiveness of a cylindrical perforated liner with varying mean bias flo...
International audienceWith regard to the reduction of aircraft noise, so-called acoustic liners are ...
The optimized design of bias flow liner is a key element for the development of low emission combust...
Interest in characterization of the aerodynamic drag of acoustic liners has increased in the past se...
Interest in the characterization of the aerodynamic drag performance of acoustic liners has increase...
Over the past several years, the NASA Langley Liner Physics Team has worked to develop methods capab...
In this study, the concept of a zero mass flow liner is evaluated. The concept enables impedance con...
The Zero Mass Flow Liner is able to convert a perforated liner with minimal damping qualities into a...
Modern aero-engines require due to their architecture an enhanced damping performance of passive, ac...
This thesis is motivated by the need for noise control in aircraft engine with orifices and perforat...
Because communities are impacted by steady increases in aircraft traffic, aircraft noise continues t...
The aerodynamic drag of acoustic liners has become a significant topic in the design of such for air...
The study of normal impedance of perforated plate acoustic liners including the effect of bias flow ...
In the field of noise reduction of aero-engines passive acoustic silencers, so-called liners still s...
Modern, low-emission aero-engine concepts, such as, for instance, Ultrahigh-Bypass Ratio (UHBR) desi...
Through this project, the effectiveness of a cylindrical perforated liner with varying mean bias flo...
International audienceWith regard to the reduction of aircraft noise, so-called acoustic liners are ...
The optimized design of bias flow liner is a key element for the development of low emission combust...
Interest in characterization of the aerodynamic drag of acoustic liners has increased in the past se...
Interest in the characterization of the aerodynamic drag performance of acoustic liners has increase...
Over the past several years, the NASA Langley Liner Physics Team has worked to develop methods capab...