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Another variation of the turboramjet does without the core inlet and the core compressor altogether.
The fan is generally placed in front of the core inlet so that the air entering the core first passes through the fan and is partially compressed by it.
Gas and liquid enter a T-section right before the core inlet line.
The core inlet flow and temperature distributions were obtained from computational fluid dynamics (CFD) simulations.
The influence of the gas entrainment is evaluated using the void fraction at the core inlet.
280 °C will be a proper temperature selected for the core inlet.
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The left of the long core represents inlet, and the right is the outlet.
Calculated results include the flow velocity and temperature fields in the core sectors, inlet and exit ducts and upper and lower plenums.
This model solves the advection diffusion equation while taking into account back diffusion from the clay core to the inlet and from the outlet to the clay core.
Results have shown that the temperature difference between core outlet and inlet is about 18°C and in this situation flow rate is about 0.004 kg/s.
The stability experiments were extended to include a hypothetical parameter range (double-void reactivity coefficient and inlet core subcooling increased by a factor of 3.6) in order to identify instability phenomena.
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