sea surface wind field model 海面风场模型
The paper introduced a spinning model surface pressure measurement sy which used in the wind tunnel.
本文介绍了可用于测量风洞中旋转模型表面压力分布的集成测试系统。
The instantaneous wind pressures on the model surface were obtained from the synchronous multi-channel pressure measurements.
模型表面的瞬态风压利用多通道同步压力测量而得到。
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。
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