Jones, Michael G. and Watson, W. R. and Howerton, B. M. and Busse-Gerstengarbe, St. (2015) Effects of Mean Flow Assumption and Harmonic Distortion on Impedance Eduction Methods. AIAA Journal, pp. 1-12. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J053399. ISSN 0001-1452.
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Abstract
This investigation uses methods based on the Pridmore-Brown and convected Helmholtz equations to study the acoustic behavior of a single-layer, conventional liner fabricated by DLR, German Aerospace Center and tested in the NASA Langley Grazing Flow Impedance Tube. Two key assumptions are explored in this investigation. First, a comparison of results achieved with uniform-flow and shear-flow impedance eduction methods is considered. Second, an approach based on the Prony method is used to extend these methods from single-mode to multimode implementations. In addition, a detailed study into the effects of harmonic distortion on the educed impedance is performed, and the results are used to develop guidelines regarding acceptable levels of harmonic distortion.
| Item URL in elib: | https://elib.dlr.de/94358/ | ||||||||||||||||||||
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| Document Type: | Article | ||||||||||||||||||||
| Title: | Effects of Mean Flow Assumption and Harmonic Distortion on Impedance Eduction Methods | ||||||||||||||||||||
| Authors: |
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| Date: | 2015 | ||||||||||||||||||||
| Journal or Publication Title: | AIAA Journal | ||||||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||||||
| Open Access: | No | ||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||||||
| DOI: | 10.2514/1.J053399 | ||||||||||||||||||||
| Page Range: | pp. 1-12 | ||||||||||||||||||||
| Publisher: | American Institute of Aeronautics and Astronautics (AIAA) | ||||||||||||||||||||
| ISSN: | 0001-1452 | ||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||
| Keywords: | Impedance eduction, harmonic distortion, liner, acoustic damping | ||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||||||||
| HGF - Program Themes: | propulsion systems | ||||||||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||||||||
| DLR - Program: | L ER - Engine Research | ||||||||||||||||||||
| DLR - Research theme (Project): | L - Turbine Technologies (old) | ||||||||||||||||||||
| Location: | Berlin-Charlottenburg | ||||||||||||||||||||
| Institutes and Institutions: | Institute of Propulsion Technology > Engine Acoustic | ||||||||||||||||||||
| Deposited By: | Bake, Dr.-Ing. Friedrich | ||||||||||||||||||||
| Deposited On: | 15 Jan 2015 14:08 | ||||||||||||||||||||
| Last Modified: | 22 Jun 2023 10:29 |
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