摘要
阐述了机身静压盘选位安装的条件，安装在机身上扰动压力为零的点位处就能探测到真实的大气静压。应用旋成体理论计算了这一点在机身上的位置，实际的安装位置是根据机身的风洞实验数据确定的，经试飞检验使用效果良好。
It introduces the conditions for the fuselage static disk to be installed through position selection. The Position where the disturbance pressure is zero will have the true atmosphere static pressure detected. By the theory of body of revolution, such position on the fuselage is calculated. The actual installation position is determined as per wind tunnel test data of the fuselage. It proves good after test flight
出处
《洪都科技》
1999年第3期16-20,共5页
Hongdu Science and Technology
