This paper provides an overview of liner research being conducted by members of the International Forum for Aviation Research (IFAR). The IFAR consists of representatives from a number of national research labs and is established to enable information exchange on aviation research activities. NASA has provided three challenges that explore different aspects of acoustic liner research, and will compile the results from each of the partners into a common database when the challenges are completed. The goal of the first challenge is to compare experimental methods applied at different national labs for acoustic liner evaluation, and to compare impedance eduction methodologies for uniform liners. The second challenge is to evaluate the ability ...
Four liners are investigated experimentally via tests in the NASA Langley Grazing Flow Impedance Tub...
As part of a cooperation between ONERA and NASA, the liner impedance eduction methods developed by t...
A number of methods have been developed at NASA Langley Research Center for eduction of the acoustic...
Three perforate-over-honeycomb liner configurations, one uniform and two with spanwise variable impe...
This paper presents the contribution from the German Aerospace Center (DLR) to the first liner bench...
As noise constraints become increasingly stringent, there is continued emphasis on the development o...
The work reported in this document consisted of six distinct liner technology development subtasks: ...
Over the past several years, the NASA Langley Liner Physics Team has worked to develop methods capab...
Accurate modeling tools are needed to design new engine liners capable of reducing aircraft noise. T...
The aerodynamic drag of acoustic liners has become a significant topic in the design of such for air...
Interest in the characterization of the aerodynamic drag performance of acoustic liners has increase...
This paper explores the effects of variable-depth geometry on the amount of noise reduction that can...
The absorption efficiency of acoustic liners used in aircraft engines is characterized by the acoust...
Acoustic liners in aircraft engine nacelles suppress radiated noise. Therefore, as air travel increa...
This paper presents the contribution from the German Aerospace Center (DLR) to the first challenge o...
Four liners are investigated experimentally via tests in the NASA Langley Grazing Flow Impedance Tub...
As part of a cooperation between ONERA and NASA, the liner impedance eduction methods developed by t...
A number of methods have been developed at NASA Langley Research Center for eduction of the acoustic...
Three perforate-over-honeycomb liner configurations, one uniform and two with spanwise variable impe...
This paper presents the contribution from the German Aerospace Center (DLR) to the first liner bench...
As noise constraints become increasingly stringent, there is continued emphasis on the development o...
The work reported in this document consisted of six distinct liner technology development subtasks: ...
Over the past several years, the NASA Langley Liner Physics Team has worked to develop methods capab...
Accurate modeling tools are needed to design new engine liners capable of reducing aircraft noise. T...
The aerodynamic drag of acoustic liners has become a significant topic in the design of such for air...
Interest in the characterization of the aerodynamic drag performance of acoustic liners has increase...
This paper explores the effects of variable-depth geometry on the amount of noise reduction that can...
The absorption efficiency of acoustic liners used in aircraft engines is characterized by the acoust...
Acoustic liners in aircraft engine nacelles suppress radiated noise. Therefore, as air travel increa...
This paper presents the contribution from the German Aerospace Center (DLR) to the first challenge o...
Four liners are investigated experimentally via tests in the NASA Langley Grazing Flow Impedance Tub...
As part of a cooperation between ONERA and NASA, the liner impedance eduction methods developed by t...
A number of methods have been developed at NASA Langley Research Center for eduction of the acoustic...