Based on the experimental observations, the vortex system model for such an airfoiltest was established.
通过实验观察假设了端板翼型实验的涡系模型。
2
Although it is very small in size, some developments in the test section of pressure distribution on airfoil surface have been attempted.
尽管该风洞的尺寸很小，我们仍对翼型表面压力分布试验段的研制工作进行了大胆的尝试。
3
The design process of the test-bed of the low speed airfoil lift-drag force characteristic was introduced, and the experimental results of the airfoil were analyzed.