Published June 1976
| Published
Journal Article
Open
Effect of flow on the acoustic reflection coefficient at a duct inlet
- Creators
- Bohn, M. S.
- Zukoski, E. E.
Chicago
Abstract
The effect of duct Mach number upon the acoustic reflection coefficient at the inlet of a duct with mean flow is investigated. An analysis, which models the duct inlet as a very short, one-dimensional nozzle over which the mean flow is accelerated from rest, gives good agreement with some recent experimental results. Discrepancies between the analysis and the experimental results are discussed in terms of radiation losses at the inlet and real fluid-flow effects within the duct.
Additional Information
© 1976, Received 9 February 1976.Attached Files
Published - 232_Bohn_MS_1976.pdf
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232_Bohn_MS_1976.pdf
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Additional details
- Eprint ID
- 21419
- Resolver ID
- CaltechAUTHORS:20101217-092218676
- Created
-
2010-12-20Created from EPrint's datestamp field
- Updated
-
2021-11-09Created from EPrint's last_modified field
- Caltech groups
- Guggenheim Jet Propulsion Center
- Other Numbering System Name
- Guggenheim Jet Propulsion Center