We studied fuel atomization in an air-assisted atomizer of aircraft engine with volume-of-fluid method in microgravitation approximation under the conditions closer to the ones of the operating cruise mode. The problem was looked upon in a two-dimensional axisymmetric configuration, including the simulation of the swirl velocity and in a three-dimensional configuration. We found a drop-size distribution function and spatial distribution of kerosene in an atomizer, which was designed by the engineers from UEC-Aviadvigatel JSC. We have hypothesized the formula connecting the drop-size distribution function obtained in the three-dimensional configuration with the distribution function obtained in the two-dimensional configuration. Along with that, the spray half angles found in these configurations appeared to be the same, although, generally, there is a difference in spatial distribution of kerosene drops.
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Univ Carlos III Madrid, Dept Ingn Term & Fluidos, Area Mecan Fluidos, Avda Univ 30, Leganes 28911, SpainUniv Carlos III Madrid, Dept Ingn Term & Fluidos, Area Mecan Fluidos, Avda Univ 30, Leganes 28911, Spain
Chakraborty, I.
Rubio-Rubio, M.
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Univ Carlos III Madrid, Dept Ingn Term & Fluidos, Area Mecan Fluidos, Avda Univ 30, Leganes 28911, SpainUniv Carlos III Madrid, Dept Ingn Term & Fluidos, Area Mecan Fluidos, Avda Univ 30, Leganes 28911, Spain
Rubio-Rubio, M.
Sevilla, A.
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Univ Carlos III Madrid, Dept Ingn Term & Fluidos, Area Mecan Fluidos, Avda Univ 30, Leganes 28911, SpainUniv Carlos III Madrid, Dept Ingn Term & Fluidos, Area Mecan Fluidos, Avda Univ 30, Leganes 28911, Spain
Sevilla, A.
Gordillo, J. M.
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Univ Seville, Dept Ingn Aeroespacial & Mecan Fluidos, Area Mecan Fluidos, Avda Descubrimientos S-N, Seville 41092, SpainUniv Carlos III Madrid, Dept Ingn Term & Fluidos, Area Mecan Fluidos, Avda Univ 30, Leganes 28911, Spain