The flight test results show that the Stripe-A-Tube method is as more effective as measurement that transform hole of static pressure on wing surface.
试飞结果表明，机翼蒙皮直接改装测量孔和测压带方法均能有效测量机翼表面压力分布。
The pressure field measurement results on the wing surface of airplane model by luminescence pressure sensor (LPS) technique and classic tap technique in high speed wind tunnel are presented.
介绍了国内首次在高速风洞中使用荧光压力传感器(LPS)技术对飞机模型机翼表面压力场测量的初步结果。
The speed fields and circulation distribution of wing-pylon combination, and the surface pressure distributions of the stores are given.
给出了机翼—挂架组合体的速度场，环量分布和外挂表面的压强分布。
The speed fields and circulation distribution of wing-pylon combination, and the surface pressure distributions of the stores are given.
给出了机翼—挂架组合体的速度场，环量分布和外挂表面的压强分布。
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