Passive means of acoustically damping devices like perforates or - more generally - liners play an important role in industrial applications to protect the community e.g against power plant noise´. In aero-engines, Helmholtz resonator type liners serve as substantial noise abatement means in regions of cold flow. An important physical property to characterize lining devices is the impedance. Several impedance eduction methods exist in literature, most of which are mathematically complicated or need substantial computation time. This paper presents a new impedance eduction method, which is relatively simple to apply, robust, and cheap in terms of computational effort. The method is derived and validated with NASA benchmark data. Its accuracy...
Two impedance eduction methods are explored for use with data acquired in the NASA Langley Grazing F...
Current aircraft engine nacelles typically contain acoustic liners consisting of perforated sheets b...
Previously developed predictive models for impedance of single-degree-of-freedom and two-degree-of-f...
© 2015 by ASME. Liner materials are commonly used to attenuate the noise propagating through a duct ...
This paper focuses on details of impedance eduction based on grazing flow duct testing. In this indi...
A number of methods have been developed at NASA Langley Research Center for eduction of the acoustic...
The need to minimize fan noise radiation from commercial aircraft engine nacelles continues to provi...
Presented here is the development of a predictive model for impedance of single-degree-of-freedom (S...
An impedance eduction technique, previously validated for ducts with plane waves at the source and d...
Aero-engine duct noise control is one of the challenging topics to be solved in view of a more envir...
An impedance eduction technique that is based upon a numerical solution to the linearized Euler equa...
A previously developed predictive model for impedance of single-degree-of-freedom and two-degree-of-...
This paper presents the experimental results obtained with three different measurement techniques us...
A two-dimensional impedance eduction theory is extended to three-dimensional sound fields and periph...
This paper documents the application of a finite element model for the specific purpose of impedance...
Two impedance eduction methods are explored for use with data acquired in the NASA Langley Grazing F...
Current aircraft engine nacelles typically contain acoustic liners consisting of perforated sheets b...
Previously developed predictive models for impedance of single-degree-of-freedom and two-degree-of-f...
© 2015 by ASME. Liner materials are commonly used to attenuate the noise propagating through a duct ...
This paper focuses on details of impedance eduction based on grazing flow duct testing. In this indi...
A number of methods have been developed at NASA Langley Research Center for eduction of the acoustic...
The need to minimize fan noise radiation from commercial aircraft engine nacelles continues to provi...
Presented here is the development of a predictive model for impedance of single-degree-of-freedom (S...
An impedance eduction technique, previously validated for ducts with plane waves at the source and d...
Aero-engine duct noise control is one of the challenging topics to be solved in view of a more envir...
An impedance eduction technique that is based upon a numerical solution to the linearized Euler equa...
A previously developed predictive model for impedance of single-degree-of-freedom and two-degree-of-...
This paper presents the experimental results obtained with three different measurement techniques us...
A two-dimensional impedance eduction theory is extended to three-dimensional sound fields and periph...
This paper documents the application of a finite element model for the specific purpose of impedance...
Two impedance eduction methods are explored for use with data acquired in the NASA Langley Grazing F...
Current aircraft engine nacelles typically contain acoustic liners consisting of perforated sheets b...
Previously developed predictive models for impedance of single-degree-of-freedom and two-degree-of-f...