哪位大神可不可以帮我翻译成英语,谢谢了!通过相关数值模拟,可以发现顶角为30度的加力燃烧室v型火焰稳定器能够更好的发挥功效.并且,加力燃烧室进口气流的静温,流速以及喷嘴喷油燃料均

哪位大神可不可以帮我翻译成英语,谢谢了!通过相关数值模拟,可以发现顶角为30度的加力燃烧室v型火焰稳定器能够更好的发挥功效.并且,加力燃烧室进口气流的静温,流速以及喷嘴喷油燃料均
哪位大神可不可以帮我翻译成英语,谢谢了!
通过相关数值模拟,可以发现顶角为30度的加力燃烧室v型火焰稳定器能够更好的发挥功效.并且,加力燃烧室进口气流的静温,流速以及喷嘴喷油燃料均会对火焰稳定器后方的流场以及温度场产生一定影响.因此,合适的进口参数将会显著提升加力燃烧室的总压恢复系数以及燃烧效率.

哪位大神可不可以帮我翻译成英语,谢谢了!通过相关数值模拟,可以发现顶角为30度的加力燃烧室v型火焰稳定器能够更好的发挥功效.并且,加力燃烧室进口气流的静温,流速以及喷嘴喷油燃料均
标准翻译：
By conducting relevant numerical simulation,it was found that the V-shaped flame stabilizer of the after-burner with an apex angle of 30 degrees can perform with better efficiency.Besides,the static temperature of the air current at the inlet of the after-burner,its flow rate and the nozzle jet fuel can also have some impact on the flow field and temperature field at the rear of the flame stabilizer.Therefore,suitable inlet parameters can significantly enhance the total pressure recovery coefficient and the combustion efficiency.

Through numerical simulation, can be found in 30 degree angle for afterburner combustion room type V flame stabilizer can play a better efficacy. And, after burning the static temperature chamber inle...

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Through numerical simulation, can be found in 30 degree angle for afterburner combustion room type V flame stabilizer can play a better efficacy. And, after burning the static temperature chamber inlet airflow, velocity and nozzle fuel injection fuel will be the flame stabilizer rear flow field and the temperature field has certain influence. Therefore, the import parameters will be appropriate to significantly improve the total pressure recovery coefficient and the afterburner combustion efficiency.

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Through relevant numerical simulation of the apex Angle of 30 degrees can be found after-burners v-shaped flame holder can better work. And reheater inlet air static temperature, velocity and nozzle i...

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Through relevant numerical simulation of the apex Angle of 30 degrees can be found after-burners v-shaped flame holder can better work. And reheater inlet air static temperature, velocity and nozzle injection fuel will flow field and temperature field of flame stabilizer rear impact. Therefore, proper import parameter after-burners will greatly increase the total pressure recovery coefficient and the combustion efficiency.

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