The results show that total pressure recovery coefficient of this type inlet is increased in every yawed flight,and are less related to the yaw angle.

 
  • 研究結果表明,這類(lèi)進(jìn)氣道在各種側滑狀態(tài)下總壓恢復系數較高,且與側滑角的關(guān)系不大。
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