在计算区域的进口处给定均匀来流速度，在出口引入压力边界条件。
Uniform incoming fluid flowing velocity is set for entry of computation region and pressure boundary condition is inducted for outlet.
从理论解可以看出，探头电极间的感应电动势与来流速度之间呈明显的线性关系。
The theoretical solutions show a clear linear relationship between the flow induced potential produced on the probe electrodes and the approach velocity.
最后确定了壁板的颤振边界，分析了温度、来流速度等因素对壁板颤振特性的影响规律。
The panel flutter boundaries are finally determined and the effect of temperature, airflow speed, etc, on the panel flutter characteristics is analyzed.
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