为此，设计了大攻角旋转天平支撑系统，此系统可测定飞机模型在不同姿态角下绕风轴以一系列恒定的角速率旋转时的气动特性。
The paper has introduced design of the support system for rotary balance of high attack angle, and the importance and methods of studying spin of aircraft.
旋转运动是由曲柄、三角架导向轴完成的。
Rotation is realized by the brace and the triangle oriented axis.
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