Published January 1976
| Published
Journal Article
Open
Experiments concerning the response of supersonic nozzles to fluctuating inlet conditions
- Creators
- Zukoski, E. E.
- Auerbach, J. M.
Abstract
The noise field produced by the passage of pressure and entropy fluctuations through a supersonic nozzle has been investigated in an experimental program. Magnitude and phase information for the disturbances produced within the nozzle are presented and are compared with numerical calculations.
Additional Information
© 1976 ASME. Received December 2, 1974. Contributed by the Gas Turbine Division and presented at the Gas Turbine Conference, Houston, Texas, March 2-6, 1975, of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS. Manuscript received at ASME headquarters December 2,1974. Paper No. 75-GT-40.Attached Files
Published - 231_Zukoski_EE_1976.pdf
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231_Zukoski_EE_1976.pdf
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Additional details
- Eprint ID
- 21415
- Resolver ID
- CaltechAUTHORS:20101217-080309933
- 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
- Paper No.
- Other Numbering System Identifier
- 75-GT-40