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(fēng)洞中使用熒光壓力傳感器(LPS)技術(shù)對飛機模型機翼表面壓力場(chǎng)測量的初步結果。
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