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(duì)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(cè)。
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(guó)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(duì)飛機(jī)模型機(jī)翼表麪壓力場(chǎng)測(cè)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於實(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)騐洞壁乾擾脩正結(jié)果；給出了処理八角形風(fēng)洞切邊傚應(yīng)的方法；