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Acoustic source location in a jet-blown flap using a cross-correlation techniqueThe acoustic source strength distribution in a turbulent flow field was measured for two far field microphones at 45 deg above and below the plane of the flap surface. A processed signal from an inclined hot-film anemometry probe was cross correlated with the signal from the appropriate far field microphone. The contribution made by the sources associated with the fluctuating pressure on the flap surface to the sound received at far field microphone was estimated by cross correlating the processed signals of microphones which were embedded in the flap surface with the far field microphone signals. In addition, detailed fluid dynamic measurements were made in the flow field of the jet flap using dual sensor hot-film anemometry probes.
Document ID
19770010886
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Becker, R. S.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Maus, J. R.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1977
Subject Category
Acoustics
Report/Patent Number
NASA-CR-149589
Report Number: NASA-CR-149589
Accession Number
77N17830
Funding Number(s)
CONTRACT_GRANT: NGR-43-001-135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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