The uniform design and response surface methodology(RSM) are applied to the multi-objective optimization of a 2-D mixed compression scramjet inlet.

 
  • 基于響應面法進(jìn)行了二維混合壓縮超燃沖壓發(fā)動(dòng)機進(jìn)氣道的多目標優(yōu)化研究。
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