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.
Numerical Modeling Of Two-Phase, Reactive Flows
NASA Tech Briefs ; 12 , 11
1988-12-01
Sonstige
Keine Angabe
Englisch
The numerical simulation of compressible reactive flows
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