Culick, F. E. C. and Magiawala, K. (1978) Measurements of Energy Losses Associated with Interactions Between Acoustic Waves and a Steady Flow Field. California Institute of Technology , Pasadena, CA. (Unpublished) https://resolver.caltech.edu/CaltechAUTHORS:20141017-143920713
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Abstract
An experimental program has been conducted to study interactions between acoustic waves and non-uniform flow fields. Data have been taken in an impedance tube, modified to accommodate an average flow, and in a resonance tube. Results are given for the influence of flow through a subsonic exhaust vent on an acoustic field. Measurements for circular and slot vents of several sizes and for two frequencies show that the flow through the vent causes a transfer of energy from the average flow field to the acoustic field: The vent acts as a source or gain of acoustic energy.
| Item Type: | Report or Paper (Technical Report) | ||||
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| Additional Information: | © 1978 California Institute of Technology. AFRPL-TR-78-6. Final Report for Period 16 March 1976- 15 November 1977. This report was submitted by Daniel and Florence Guggenheim Jet Propulsion Center, California Institute of Technology, Pasadena, California 91 125, under Contract No. F04611-75-C-0010, Job Order No. 573010AU with the Air Force Rocket Propulsion Laboratory, Edwards AF B, California 93523. | ||||
| Group: | GALCIT | ||||
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| Subject Keywords: | Combustion Instability, T-Burners, Acoustics, Solid Propellant Rockets | ||||
| Record Number: | CaltechAUTHORS:20141017-143920713 | ||||
| Persistent URL: | https://resolver.caltech.edu/CaltechAUTHORS:20141017-143920713 | ||||
| Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. | ||||
| ID Code: | 50505 | ||||
| Collection: | CaltechAUTHORS | ||||
| Deposited By: | INVALID USER | ||||
| Deposited On: | 20 Oct 2014 15:48 | ||||
| Last Modified: | 03 Oct 2019 07:24 |
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