high pressure wind tunnel

基本解釋

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(fēng)洞氣源氣罐全厚材料用超聲、磁粉、射線等方法進(jìn)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(nèi)首次在高速風(fēng)洞中使用熒光壓力傳感器（LPS）技術(shù)對飛機(jī)模型機(jī)翼表面壓力場測量的初步結(jié)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于實(shí)壁低速八角形風(fēng)洞，獲得了一個(gè)三維模型大攻角實(shí)驗(yàn)洞壁干擾修正結(jié)果；給出了處理八角形風(fēng)洞切邊效應(yīng)的方法；