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Laboratory studies of lean combustionThe fundamental processes controlling lean combustion were observed for better understanding, with particular emphasis on the formation and measurement of gas-phase pollutants, the stability of the combustion process (blowout limits), methods of improving stability, and the application of probe and optical diagnostics for flow field characterization, temperature mapping, and composition measurements. The following areas of investigation are described in detail: (1) axisymmetric, opposed-reacting-jet-stabilized combustor studies; (2) stabilization through heat recirculation; (3) two dimensional combustor studies; and (4) spectroscopic methods. A departure from conventional combustor design to a premixed/prevaporized, lean combustion configuration is attractive for the control of oxides of nitrogen and smoke emissions, the promotion of uniform turbine inlet temperatures, and, possibly, the reduction of carbon monoxide and hydrocarbons at idle.
Document ID
19780003136
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sawyer, R. F.
(California Univ. Berkeley, CA, United States)
Schefer, R. W.
(California Univ. Berkeley, CA, United States)
Ganji, A. R.
(California Univ. Berkeley, CA, United States)
Daily, J. W.
(California Univ. Berkeley, CA, United States)
Pitz, R. W.
(California Univ. Berkeley, CA, United States)
Oppenheim, A. K.
(California Univ. Berkeley, CA, United States)
Angeli, J. W.
(California Univ. Berkeley, CA, United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1977
Publication Information
Publication: NASA. Lewis Res. Center Aircraft Eng. Emissions
Subject Category
Aircraft Propulsion And Power
Accession Number
78N11079
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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