The later coming test work will help further validating and correcting. It is significant for the design calculation of a pressure-swirl nozzle with oil returning channel.
本文接下去的设计计算将通过试验验证、修正，为离心回油式喷嘴计算提供一定的借鉴。
The method can be used for combustion Chambers with any shape to match the fuel injection pressure, nozzle construction, injector position and intake swirl ratio with chamber shape.
该方法可适于任意形状的燃烧室，能反映出喷油压力、喷油嘴结构及安装位置、进气涡流比等参数与燃烧室形状的匹配关系。
The re- search provides an important experimental basis for the design and improvement of swirl pressure nozzle.
实验结果可以为旋流压力式喷嘴设计和改进提供重要的实验依据。
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