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Fan Noise Source Diagnostic Test: Vane Unsteady Pressure ResultsTo investigate the nature of fan outlet guide vane pressure fluctuations and their link to rotor-stator interaction noise, time histories of vane fluctuating pressures were digitally acquired as part of the Fan Noise Source Diagnostic Test. Vane unsteady pressures were measured at seven fan tip speeds for both a radial and a swept vane configuration. Using time-domain averaging and spectral analysis, the blade passing frequency (BPF) harmonic and broadband contents of the vane pressures were individually analyzed. Significant Sound Pressure Level (SPL) reductions were observed for the swept vane relative to the radial vane for the BPF harmonics of vane pressure, but vane broadband reductions due to sweep turned out to be much smaller especially on an average basis. Cross-correlation analysis was used to establish the level of spatial coherence of broadband pressures between different locations on the vane and integral length scales of pressure fluctuations were estimated from these correlations. Two main results of this work are: (1) the average broadband level on the vane (in dB) increases linearly with the fan tip speed for both the radial and swept vanes, and (2) the broadband pressure distribution on the vane is nearly homogeneous and its integral length scale is a monotonically decreasing function of fan tip speed.
Document ID
20020084621
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Envia, Edmane
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2002
Subject Category
Acoustics
Report/Patent Number
NASA/TM-2002-211808
NAS 1.15:211808
E-13503
AIAA Paper 2002-2430
Report Number: NASA/TM-2002-211808
Report Number: NAS 1.15:211808
Report Number: E-13503
Report Number: AIAA Paper 2002-2430
Meeting Information
Meeting: Eighth Aeroacoustics Conference
Location: Breckenridge, CO
Country: United States
Start Date: June 17, 2002
End Date: June 19, 2002
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies
Funding Number(s)
PROJECT: RTOP 781-30-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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