The suggested surface can increase the aerodynamic efficiency (lift-to-drag ratio) of the baseline configuration by 5%-6% in subsonic and supersonic flight regimes.

 
  • 此外,不論是亞聲速還是超聲速飛行,氣動(dòng)操縱面均可以提高氣動(dòng)效率5%25-6%25。
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