The influence of blade thickness and torsion on the flow field at low Reynolds number for rotor in a hover is studied with the Chimera grid technique.

 
  • 摘要運用嵌套網(wǎng)格技術(shù)研究了漿葉的厚度和扭轉對低雷諾數旋翼流場(chǎng)的影響。
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