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A laser-induced-fluorescence visualization study of transverse, sonic fuel injection in a nonreacting supersonic combustorThe present paper reports work which has been conducted in the first phase of a research program which is to provide a data base of spatially-resolved measurements in nonreacting supersonic combustors. In the measurements, a nonintrusive diagnostic technique based on the utilization of laser-induced fluorescence (LIF) is employed. The reported work had the objective to conduct LIF visualization studies of the injection of a simulated fuel into a Mach 2.07 airstream for comparison with corresponding numerical calculations. Attention is given to injection from a single orifice into a constant-area duct, injection from a single orifice behind a rearward-facing step, and injection from staged orifices behind a rearward-facing step.
Document ID
19860041905
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcdaniel, J. C.
(Virginia Univ. Charlottesville, VA, United States)
Graves, J., Jr.
(Virginia, University Charlottesville, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 86-0507
Accession Number
86A26643
Funding Number(s)
CONTRACT_GRANT: NAG1-373
Distribution Limits
Public
Copyright
Other

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