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A numerical study is performed to investigate the effect of preshock turbulence on the detonation wave properties. The analysis is based on the integration of the chemically reactive Navier–Stokes equations using a Runge–Kutta scheme and a fifth-order WENO spatial discretization. The results show a marked influence of preshock perturbations on the postshock statistics. The alteration to the limit...
A theoretical investigation of the coupling between the core flow process and combustion sublayer process in a rocket chamber flow is presented. The focus of the investigation is on penetration of chamber disturbances into the sublayer and on the burn rate characteristic responses. Characteristic solutions to the local non-parallel instability problem supported by gasifying propellant in a double...
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