Finally, the aircraft CJ818 is designed for relaxed static stability and the meliorative result has been shown.

 
  • 最后,論文以CJ818飛機為例,進(jìn)行了放寬縱向靜穩定性設計,并對設計優(yōu)化后的飛機構型進(jìn)行了氣動(dòng)性能評估。
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