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分别以固壁条件和洞壁附近的压力分布模拟各类实壁和透气壁试验段的洞壁边界条件，利用Euler方程和N－S方程数值求解模型在风洞中的绕流场，得出洞壁干扰对跨声速模型统流和气动力的影响。初步的研究结果表明，该方法能较有效地模拟模型在跨声速风洞中的绕流场，经洞壁干扰修正后的GBM－04A模型在0．6m风洞中的试验结果与无干扰参考结果吻合较好。
The wall boundary conditions of various types of solid wall and breathable wall were simulated by the solid wall conditions and the pressure distribution near the wall respectively. The Euler equation and N-S equation were used to solve the flow field in the wind tunnel. Influence of Tunnel Wall Disturbance on the Interaction and Aerodynamics of Transonic Model. The preliminary results show that this method can simulate the flow around the model in a transonic wind tunnel more effectively. The test results of the GBM-04A model modified by the interference of the wall in a 0.6 m wind tunnel can be compared with the non-interference reference The result is in good agreement.