Considering the features of solid rocket motor jet, a kind of experimental equipment based on the pitot tube technology for measuring the multi-point pressures was developed.

 
  • 結合固體火箭燃氣射流的特點(diǎn),開(kāi)發(fā)了基于皮托管技術(shù)的多點(diǎn)壓力參數實(shí)驗測量裝置,運用實(shí)驗的方法,對燃氣射流流場(chǎng)進(jìn)行了研究。
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