A new computational fluid dynamics code has been developed for the study of mixing and chemical reactions in the flow fields of ramjets and scramjets. The code employs an implicit finite-volume, lower-upper symmetric successive overrelaxation (LU-SSOR) scheme for solving the complete two-dimensional Navier-Stokes equations and species transport equations in a fully coupled and very efficient manner. The combustion processes are modeled by an 8-species, 14-step, finite-rate chemistry model, and the turbulence is simulated by a Baldwin-Lomax algebraic model
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