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Analytical Modeling of Operating Characteristics of Premixing-prevaporizing Fuel-air Mixing PassagesA model for predicting the distribution of liquid fuel droplets and fuel vapor in premixing-prevaporizing fuel-air mixing passages of the direct injection type is described. This model consists of three computer programs: a calculation of the two dimensional or axisymmetric air flow field neglecting the effects of fuel; a calculation of the three dimensional fuel droplet trajectories and evaporation rates in a known, moving air flow; and a calculation of fuel vapor diffusing into a moving three dimensional air flow with source terms dependent on the droplet evaporation rates. The air flow calculation can treat compressible swirling flows in arbitrary ducts with arbitrary distributions of temperature and velocity as initial conditions. The fuel droplets are treated as initial conditions. The fuel droplets are treated as individual particle classes each satisfying Newton's law, a heat transfer, and a mass transfer equation. The vapor diffusion calculation treats three dimensional, gas phase, turbulent diffusion processes with the turbulence level determined by the air flow calculations and the source terms determined by the droplet evaporation rates.
Document ID
19830020938
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, O. L.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1983
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Aircraft Propulsion And Power
Accession Number
83N29209
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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