NASA NTRS · 19850000376
Predicting Two-Dimensional, Unsteady Turbulent Combustion
Abstract
MIMOC calculates flow field and flame propagation in turbulent combustion tunnel. Program employs algorithm for turbulent combustion modeling described by Ghoniem, Chorin, and Oppenheim. Program used to study flow field in model combustor, formed by rearward-facing step in channel, in terms of vorticity field, velocity field, turbulent shear stresses, flame contours, and concentration field.
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Marek, C. J., Ghoniem, A. F., Oppenheim, A. K.. 1986-01-01. Predicting Two-Dimensional, Unsteady Turbulent Combustion. https://ntrs.nasa.gov/citations/19850000376
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