2004Journal of Solid Rocket TechnologyRequires access

Numerical simulation and mechanism investigation on equidirectional fuel-air/oxygen mixing enhanced by synthetic jet actuators

Dequan Wang

Open publisher page 2 citations

Abstract

The overall flow field calculation model(X-L) which takes actuator cavity, exit throat and exterior flow field as a single computational region was established. Based on the calculation model, equidirectional fuel-air/oxygen mixing flow field enhanced by synthetic jet actuators was numerically simulated and investigated. The result showed that synthetic jet actuators can significantly enhance fuel-air/oxygen mixing. The main mechanism is that synthetic jet actuators controlling flow direction of fuel-air/oxygen enable the two oxygen parallel jet on both sides to deflect inwards, so as to greatly shorten core region length of every jet; at the same time, actuators alter and strengthen the vortex structure near the jet exit, and the strong convection action of the vortex structure significanfly enhances fuel-air/oxygen parallel jet mixing near the exit.

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What this paper is about

The overall flow field calculation model(X-L) which takes actuator cavity, exit throat and exterior flow field as a single computational region was established. Based on the calculation model, equidirectional fuel-air/oxygen mixing flow field enhanced by synthetic jet actuators was numerically simulated and investigated. The result showed that synthetic jet actuators can significantly enhance fuel-air/oxygen mixing. The main mechanism is that synthetic jet actuators controlling flow direction of fuel-air/oxygen enable the two oxygen parallel jet on both sides to deflect inwards, so as to greatly shorten core region length of every jet; at the same time, actuators alter and strengthen the vortex structure near the jet exit, and the strong convection action of the vortex structure significanfly enhances fuel-air/oxygen parallel jet mixing near the exit.

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Available abstract

The overall flow field calculation model(X-L) which takes actuator cavity, exit throat and exterior flow field as a single computational region was established. Based on the calculation model, equidirectional fuel-air/oxygen mixing flow field enhanced by synthetic jet actuators was numerically simulated and investigated. The result showed that synthetic jet actuators can significantly enhance fuel-air/oxygen mixing. The main mechanism is that synthetic jet actuators controlling flow direction of fuel-air/oxygen enable the two oxygen parallel jet on both sides to deflect inwards, so as to greatly shorten core region length of every jet; at the same time, actuators alter and strengthen the vortex structure near the jet exit, and the strong convection action of the vortex structure significanfly enhances fuel-air/oxygen parallel jet mixing near the exit.

Key concepts: Jet (fluid), Mechanics, Mixing (physics), Vortex, Synthetic jet, Jet fuel, Actuator, Oxygen

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