采用了一个修正的螺旋桨尾涡模型，来模拟导管螺旋桨尾涡片的扭曲变形及分离现象。
A modified trailing vortex wake model of propeller is introduced to describe the distortion and separation of the trailing vortex sheet.
本文基于一种并行高精度的静动交接面处理方法，采用了SA模型及基于SA的分离涡模拟DES方法，进行了某压气机静动干涉流动的计算。
Based on a high-accuracy and large-scale-parallel method, SA model and detached eddy simulation (DES) based on SA were employed to research the flows of compressor stator-rotor interaction.
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