论文部分内容阅读
一种适用于具有大展弦比机翼和船尾形机身的飞机模型的腹部支撑方式、腹支装置的设计要求和试验方法、以及腹支撑干扰的机理在此作了介绍，并给出了一些实验结果和对实验数据的修正方法．
An abdominal support method suitable for aircraft models with large aspect ratio airfoils and stern frames, the design requirements and test methods of ventral support devices, and the mechanism of abdominal support disturbance are presented and presented Some experimental results and methods to correct the experimental data.