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Journal: AerospaceVolume: 11Number: 46
Article: Calculation and Selection of Airfoil for Flapping-Wing Aircraft Based on Integral Boundary Layer Equations
  • Authors:
  • Ming Qi1,*,
  • Wenguo Zhu2 and
  • Shu Li1,*
Link: https://www.mdpi.com/2226-4310/11/1/46

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