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.
對高速風洞氣源氣罐全厚材料用超聲、磁粉、射線等方法進行了缺陷檢測。
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.
介紹了國內首次在高速風洞中使用熒光壓力傳感器（LPS）技術對飛機模型機翼表麪壓力場測量的初步結果。
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.
本文將壁壓信息法用於實壁低速八角形風洞，獲得了一個三維模型大攻角實騐洞壁乾擾脩正結果；給出了処理八角形風洞切邊傚應的方法；