Published 1985 | Version v1
Book

Experimental investigation of an unsteady combusting flow in a pulse combustor

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--.