NASA NTRS · 19880000576
Numerical Modeling Of Two-Phase, Reactive Flows
Abstract
Capabilities of several computational schemes combined and enhanced. Advanced Rocket Injector-Combustor Code is computer program for numerical simulation of two-phase flows of chemically reacting or nonreacting components. Applied to sprays of fuel in injectors and combustors, flows in heat exchangers, evaporators, and mass-diffusion systems; and two-dimensional or axisymmetric flows containing liquid or solid suspensions. Used in research for development and verification of various physical models.
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Liang, Pak-Yan. 1988-12-01. Numerical Modeling Of Two-Phase, Reactive Flows. https://ntrs.nasa.gov/citations/19880000576
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