Measurement of acoustic modes and wall impedance in a turbofan exhaust duct
G. H. Fiske, A.A. Syed, R. E. Motsinger, M. C. Joshi, Robert E. Kraft
Abstract
G. H. Fiske, A.A. Syed, R. E. Motsinger, M. C. Joshi, Robert E. Kraft
Abstract
Acoustic measurements made with in-duct modal probes show how individual acoustic modes, as generated by fan/stator interaction, interact with a well-characterized liner. This measured attenuation provides a critical test for predicted attenuation as developed from the theoretical analysis of sound propagation in annular ducts with treatment and sheared flow. The primary investigations took place in the exhaust duct of a model fan mounted in an anechoic chamber. The results presented include induct attenuation, sound power attenuation as measured in the far field, and in-situ acoustic impedance measurements of the treated wall sections. Good theory/experiment agreement was found; the differences of treatment suppression between theory and measured values differed at most by 2.7 dB.
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Acoustic measurements made with in-duct modal probes show how individual acoustic modes, as generated by fan/stator interaction, interact with a well-characterized liner. This measured attenuation provides a critical test for predicted attenuation as developed from the theoretical analysis of sound propagation in annular ducts with treatment and sheared flow. The primary investigations took place in the exhaust duct of a model fan mounted in an anechoic chamber. The results presented include induct attenuation, sound power attenuation as measured in the far field, and in-situ acoustic impedance measurements of the treated wall sections. Good theory/experiment agreement was found; the differences of treatment suppression between theory and measured values differed at most by 2.7 dB.
Key concepts: Turbofan, Acoustics, Duct (anatomy), Electrical impedance, Acoustic impedance, Focused Impedance Measurement, Materials science, Aerospace engineering