Segmented Liner to Control Mode Scattering

Abstract

The acoustic performance of duct liners can be improved by segmenting the treatment. In a segmented liner treatment, one stage of liner reduces the target sound and scatters energy into other acoustic modes, which are attenuated by a subsequent stage. The Curved Duct Test Rig is an experimental facility in which sound incident on the liner can be generated in a specific mode and the scatter of energy into other modes can be quantified. A series of experiments is performed in which the baseline configuration is asymmetric, that is, a liner is on one side wall of the test duct and the wall opposite is acoustically hard. Segmented liner treatment is achieved by progressively replacing sections of the hard wall opposite with liner in the axial direction, from 25% of the wall surface to 100%. It is found that the energy scatter from the (0,0) to the (0,1) mode reduces as the percentage of opposite wall treatment increases, and the frequency of peak attenuation shifts toward higher frequency. Similar results are found when the incident mode is of order (0,1) and scatter is into the (0,0) mode. The propagation code CDUCT-LaRC is used to predict the effect of liner segmenting on liner performance. The computational results show energy scatter and the effect of liner segmentation that agrees with the experimental results. The experiments and computations both show that segmenting the liner treatment is effective to control the scatter of incident mode energy into other modes. CDUCT-LaRC is shown to be a valuable tool to predict trends of liner performance with liner configuration.

Design and Acoustic Efficacy of a Broadband Liner for the Inlet of the DGEN Aero-propulsion Research Turbofan

“…To gain further confidence in the tools used within the broadband liner design process, a series of multidegree of freedom (MDOF) liner design studies at increasing technology readiness levels (TRL) have been conducted as the overall optimization methodology has been enhanced. Initial liner designs targeting the NASA Langley Liner Technology Facility 8,9 (LTF) resulted in predicted optimum impedance spectra consistent with those obtained using higher-fidelity, more computationally intensive models 10 . Subsequent design and testing in the NASA Glenn Advanced Noise Control Fan (ANCF) Rig 3,4 and 9-ft x 15-ft Low Speed Wind Tunnel 5,6 provided further confidence in the design process.…”

Broadband Inlet Liner Design for the DGEN Aero-propulsion Research Turbofan

“…To gain further confidence in the tools used within the broadband liner design process, a series of multi-degree of freedom (MDOF) liner design studies at increasing technology readiness levels (TRL) has been conducted as the overall optimization methodology has been enhanced. Initial liner designs targeting the NASA Langley Liner Technology Facility 7,8 (LTF) resulted in predicted optimum impedance spectra consistent with those obtained using higher-fidelity, more computationally intensive models. Subsequent design and testing in the NASA Glenn Advanced Noise Control Fan (ANCF) Rig 3, 4 and 9-ft x 15-ft Low Speed Wind Tunnel 5,6 provided further confidence in the design process.…”

Further Development and Assessment of a Broadband Liner Optimization Process

“…To gain confidence in the tools used within the broadband liner design process, a series of multi-degree of freedom (MDOF) liner design studies at increasing technology readiness levels (TRL) has been conducted as the overall optimization methodology has been enhanced. Initial liner designs targeting the NASA Langley Liner Technology Facility 4,5 (LTF) resulted in predicted optimum impedance spectra consistent with those obtained using higher-fidelity, more computationally intensive models. Subsequent design and testing in the NASA Glenn Advanced Noise Control Fan (ANCF) Rig 3,6 provided further confidence in the design process.…”