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Comparison of inlet suppressor data with approximate theory based on cutoff ratioInlet suppressor far-field directivity suppression was quantitatively compared with that predicted using an approximate linear design and evaluation method based upon mode cutoff ratio. The experimental data was obtained using a series of cylindrical point-reacting inlet liners on a YF102 engine. The theoretical prediction program is based upon simplified sound propagation concepts derived from exact calculations. These indicate that all of the controlling phenomenon can be approximately correlated with mode cutoff ratio which itself is intimately related to the angles of propagation within the duct. The theory-data comparisons are intended to point out possible deficiencies in the approximate theory which may be corrected. After all theoretical refinements are made, then empirical corrections can be applied.
Document ID
19800007616
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rice, E. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Heidelberg, L. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1979
Subject Category
Acoustics
Report/Patent Number
NASA-TM-81386
E-294
Report Number: NASA-TM-81386
Report Number: E-294
Meeting Information
Meeting: AIAA Aerospace Sci. Meeting
Location: Pasadena, CA
Country: United States
Start Date: January 14, 1980
End Date: January 16, 1980
Accession Number
80N15876
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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