Experimental investigation of an unsteady combusting flow in a pulse combustor
Creators
Description
Pulse combustion devices exhibit exceedingly high thermal efficiency and very low pollutant emission when used in heating applications. Application of these heating devices has been limited, however, because of a lack of understanding of the fundamental controlling physical and chemical processes governing pulse combustors. An experimental research program has been initiated at Sandia National Laboratories to develop such insight. This paper reports the results of an experiment studying the effects of changing heat release and pressure pulsations on the fluid dynamics in the combustion chamber of a square pulse combustor. Using a two-color laser Doppler velocimeter (LDV) as a diagnostic tool, this study indicates that the fluid dynamics in the combustion chamber are strongly affected by pressure pulsations and are weakly affected by a change in the heat release rate
Additional details
Publishing Information
- Publisher
- American Institute of Aeronautics and Astronautics.
- Imprint Place
- New York, NY (USA)
- Imprint Pagination
- 10 p.
Conference
- Title
- 23. AIAA aerospace sciences meeting.
- Dates
- 14-17 Jan 1985.
- Place
- Reno, NV (USA).
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 17014183
- Subject category
- S75: CONDENSED MATTER PHYSICS, SUPERCONDUCTIVITY AND SUPERFLUIDITY;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- COMBUSTION; FLUID MECHANICS; UNSTEADY FLOW; VELOCIMETERS; VORTEX FLOW
- Descriptors DEC
- CHEMICAL REACTIONS; FLUID FLOW; MEASURING INSTRUMENTS; MECHANICS; OXIDATION
Optional Information
- Secondary number(s)
- CONF-850136--.