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Power cepstrum technique with application to model helicopter acoustic dataThe application of the power cepstrum to measured helicopter-rotor acoustic data is investigated. A previously applied correction to the reconstructed spectrum is shown to be incorrect. For an exact echoed signal, the amplitude of the cepstrum echo spike at the delay time is linearly related to the echo relative amplitude in the time domain. If the measured spectrum is not entirely from the source signal, the cepstrum will not yield the desired echo characteristics and a cepstral aliasing may occur because of the effective sample rate in the frequency domain. The spectral analysis bandwidth must be less than one-half the echo ripple frequency or cepstral aliasing can occur. The power cepstrum editing technique is a useful tool for removing some of the contamination because of acoustic reflections from measured rotor acoustic spectra. The cepstrum editing yields an improved estimate of the free field spectrum, but the correction process is limited by the lack of accurate knowledge of the echo transfer function. An alternate procedure, which does not require cepstral editing, is proposed which allows the complete correction of a contaminated spectrum through use of both the transfer function and delay time of the echo process.
Document ID
19870008046
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Martin, R. M.
(NASA Langley Research Center Hampton, VA, United States)
Burley, C. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1986
Subject Category
Acoustics
Report/Patent Number
L-16070
NAS 1.60:2586
NASA-TP-2586
Report Number: L-16070
Report Number: NAS 1.60:2586
Report Number: NASA-TP-2586
Accession Number
87N17479
Funding Number(s)
PROJECT: RTOP 505-61-51-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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