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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2018
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Article
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Fig 3
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Research Article
Modeling of Spray Combustion with a Steady Laminar Flamelet Model in an Aeroengine Combustion Chamber Based on OpenFOAM
Figure 3
Profile comparison at the centerline of flame B.
(a)
Temperature
(b)
Mixing fraction
(c)
Axial velocity