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Modeling of premixing-prevaporizing fuel-air mixing passagesThe development of a computer program for the analytical prediction of the distribution of liquid and vapor fuel in the premixing-prevaporizing passage by the direct injection method is described. The technical approach adopted for this program is to separate the problem into three parts each with its own computer code. These three parts are: calculation of the two-dimensional or axisymmetric air flow; calculation of the three-dimensional fuel droplet evaporation; and calculation of the fuel vapor diffusion. This method of approach is justified because premixing passages operate at lean equivalence ratios. Hence, a weak interaction assumption can be made wherein the airflow can affect the fuel droplet behavior but the fuel droplet behavior does not affect the airflow.
Document ID
19790016827
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, O. L.
(United Technologies Research Center East Hartford, CT, United States)
Mcvey, J. B.
(United Technologies Research Center East Hartford, CT, United States)
Edwards, D. E.
(United Technologies Research Center East Hartford, CT, United States)
Chiappetta, L. M.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Lewis Res. Center Premixed Prevaporized Combustor Technol. Forum
Subject Category
Aircraft Propulsion And Power
Accession Number
79N24998
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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