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一种计算高速风洞腹部支架对模型纵横向气动力干扰量的工程方法，可以非常方便地分析腹支的位置、厚度、后掠角等几何参数对干扰量的影响。与支架干扰实验结果的比较表叨，本方法可以用作为选择腹支位置及几何外形参数的理论工具。
An engineering method for calculating the longitudinal and lateral aerodynamic interference of the model high-speed wind tunnel abdominal stent model can be very convenient to analyze the influence of the geometric parameters such as the position, thickness and sweep angle of the ventral branch on the disturbance amount. Comparison with experimental results of stent interference Table 4: This method can be used as a theoretical tool for selecting the location of abdominal veins and geometric shape parameters.