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在模拟涡轮喷气发动机加力燃烧室进口气流温度下,应用轨道扩散模型计算了直射式喷嘴跨流喷射时火焰稳定器截面燃油浓度分布。
In the simulation of turbulent jet engine afterburner inlet airflow temperature, the orbital diffusion model was used to calculate the cross-sectional fuel concentration distribution of the flame stabilizer cross-jet injection.