| Citation: | ZHANG Anjing, QIN Kan, WANG Hanwei, et al. Influence of secondary combustion reaction on the performance of air-underwater dual-mode turbines[J]. Journal of Aerospace Power, 2024, 39（10）：20220671 doi: 10.13224/j.cnki.jasp.20220671
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In order to make the trans medium vehicle adapt to underwater and air medium navigation at the same time, research on the secondary combustion reaction process of a new dual-mode turbine was carried out. The turbine used kerosene and air as fuels when it worked in the air, and used Yutui-3 propellant as fuel when it worked underwater. At the stage of turbine water take-off, kerosene and Yutui-3 propellant need to be burned at the same time. As the combustion products of Yutui-3 propellant contain a large amount of CO, H2 and CH4, it will produce secondary combustion after mixing with the residual air from kerosene combustion. In order to analyze the influence of secondary combustion reaction during takeoff, the influence of secondary combustion reaction on the performance of air-water dual-purpose turbine was studied by numerical simulation. The results showed that these two kinds of fuel gases had chemical reaction, and CO, H2 and CH4 in Yutui 3 fuel gas were almost completely burned; the secondary combustion reaction mainly occurred in the front section of the nozzle. The maximum temperature of the combustion section increased from 712 K to 2 185 K, which increased the outlet velocity of the nozzle and made the thrust increase by about 30.24%. This study provides an idea for the increase of thrust of air water turbine during takeoff.
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