The study of normal impedance of perforated plate acoustic liners including the effect of bias flow was studied. Two impedance models were developed by modeling the internal flows of perforate orifices as infinite tubes with the inclusion of end corrections to handle finite length effects. These models assumed incompressible and compressible flows, respectively, between the far field and the perforate orifice. The incompressible model was used to predict impedance results for perforated plates with percent open areas ranging from 5% to 15%. The predicted resistance results showed better agreement with experiments for the higher percent open area samples. The agreement also tended to deteriorate as bias flow was increased. For perforated pla...
The need to minimize fan noise radiation from commercial aircraft engine nacelles continues to provi...
A two-dimensional impedance eduction theory is extended to three-dimensional sound fields and periph...
The present work explored the feasibility of controlling the acoustic impedance of a resonant type a...
A new bias flow impedance model is developed for perforated plates from basic principles using as li...
An experimental investigation was conducted to generate a high quality database, from which the effe...
Previously developed predictive models for impedance of single-degree-of-freedom and two-degree-of-f...
A previously developed predictive model for impedance of single-degree-of-freedom and two-degree-of-...
This thesis is motivated by the need for noise control in aircraft engine with orifices and perforat...
Perforates are for instance used in mufflers for automotive applications and in acoustic liners for ...
Presented here is the development of a predictive model for impedance of single-degree-of-freedom (S...
Through this project, the effectiveness of a cylindrical perforated liner with varying mean bias flo...
In this study, the concept of a zero mass flow liner is evaluated. The concept enables impedance con...
Current aircraft engine nacelles typically contain acoustic liners consisting of perforated sheets b...
This paper presents results of an investigation of the effects of shear flow profile on impedance ed...
This paper focuses on details of impedance eduction based on grazing flow duct testing. In this indi...
The need to minimize fan noise radiation from commercial aircraft engine nacelles continues to provi...
A two-dimensional impedance eduction theory is extended to three-dimensional sound fields and periph...
The present work explored the feasibility of controlling the acoustic impedance of a resonant type a...
A new bias flow impedance model is developed for perforated plates from basic principles using as li...
An experimental investigation was conducted to generate a high quality database, from which the effe...
Previously developed predictive models for impedance of single-degree-of-freedom and two-degree-of-f...
A previously developed predictive model for impedance of single-degree-of-freedom and two-degree-of-...
This thesis is motivated by the need for noise control in aircraft engine with orifices and perforat...
Perforates are for instance used in mufflers for automotive applications and in acoustic liners for ...
Presented here is the development of a predictive model for impedance of single-degree-of-freedom (S...
Through this project, the effectiveness of a cylindrical perforated liner with varying mean bias flo...
In this study, the concept of a zero mass flow liner is evaluated. The concept enables impedance con...
Current aircraft engine nacelles typically contain acoustic liners consisting of perforated sheets b...
This paper presents results of an investigation of the effects of shear flow profile on impedance ed...
This paper focuses on details of impedance eduction based on grazing flow duct testing. In this indi...
The need to minimize fan noise radiation from commercial aircraft engine nacelles continues to provi...
A two-dimensional impedance eduction theory is extended to three-dimensional sound fields and periph...
The present work explored the feasibility of controlling the acoustic impedance of a resonant type a...