Computation Of Ramjet Internal Flowfields
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Computation of Ramjet Internal Flowfields
This document reports on the computation of Ramjet Internal Flowfields. It is divided into two sections, i.e. subsonic and supersonic combustion. To numerically simulated subsonic combustion the time-dependent Navier-Stokes equations are used with additional species equations incorporated to model hydrocarbon-air combustion. To compute supersonic combustion the parabolized Navier-Stokes equations are utilized (PNS) with species equations to simulate hydrogen-air combustions. Model cases are computed and compared with limited experimental data. Keywords: PNS; Ramjet; Scramjet engines; Computational fluids; Dynamics. (AW).