Effects of C/O Ratio and Temperature on Sooting Limits of Spherical Diffusion Flames
Author(s) -
Vivien Lecoustre,
Peter B. Sunderland,
B.H. Chao,
David L. Urban,
Dennis P. Stocker,
Richard L. Axelbaum
Publication year - 2008
Publication title -
45th aiaa aerospace sciences meeting and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2008-827
Subject(s) - diffusion , materials science , thermodynamics , aspect ratio (aeronautics) , physics , composite material
‡‡ Limiting conditions for soot particle inception in spherical diffusion flames were investigated numerically. The flames were modeled using a one-dimensional, time accurate diffusion flame code with detailed chemistry and transport and an optically thick radiation model. Seventeen normal and inverse flames were considered, covering a wide range of stoichiometric mixture fraction, adiabatic flame temperature, residence time and scalar dissipation rate. These flames were previously observed to reach their sooting limits after 2 s of microgravity. Sooting-limit diffusion flames with scalar dissipation rate lower than 2 s -1 were found to have temperatures near 1400 K where C/O = 0.51, whereas flames with greater scalar dissipation rate required increased temperatures. This finding was valid across a broad range of fuel and oxidizer compositions and convection directions.
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