Experimental Investigation on the Flow and Heat Transfer Characteristics of Aviation Kerosene RP-3 During Thermal Pyrolysis Coking[J]. 2016, 50(7): 7-12.
DOI:
Experimental Investigation on the Flow and Heat Transfer Characteristics of Aviation Kerosene RP-3 During Thermal Pyrolysis Coking[J]. 2016, 50(7): 7-12.DOI: 10.7652/xjtuxb201607002.
Experimental Investigation on the Flow and Heat Transfer Characteristics of Aviation Kerosene RP-3 During Thermal Pyrolysis Coking
The flow and heat transfer characteristics of aviation kerosene RP-3 during its pyrolysis coking in a Φ3 mm×0.5 mm high-temperature alloy steel tube were investigated to understand the influence of coking in the regenerative thermal protection structures of scramjet on heat transfer. Experiments were conducted at the pressure of 3 MPa
the mass flow rate of 0.5 g·s
-1
and the heat fluxes of 325
365 and 374 kW·m
-2
. The discrepancy of convection heat transfer characteristics in the tube before and after coking was discussed. It was found that there occurred an abrupt pressure drop in the test tube section during coking test and the external wall temperature was reduced gradually du
ring the thermal pyrolysis. These results revealed that coking was an unstable process with the coke depositing and removing. The coking rate would increase with the wall temperature. Coking might form porous surface on the inner wall of the tube
which would enhance the pseudo boiling heat transfer under the supercritical pressure condition when the temperature of the fluid near the wall was close to or higher than the pseudo critical temperature. However
when the temperature of the fluid near the wall was too low to maintain pseudo boiling
a heat transfer deterioration would occur because of the thermal resistance effect of the coking layer.
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references
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