high pressure wind tunnel

基本解释

Defect on air pressure vessel materials of high speed wind tunnel resource was inspected by means of ultrasonic radiographic and magnetic particle.
对高速风洞气源气罐全厚材料用超声、磁粉、射线等方法进行了缺陷检测。
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。
Wall pressure signature m'ethod has been applied to wall correction for three-dimensional models at high angles of attack in low-speed wind tunnel with a closed octagonal test section.
本文将壁压信息法用于实壁低速八角形风洞，获得了一个三维模型大攻角实验洞壁干扰修正结果；给出了处理八角形风洞切边效应的方法；