EXAMPLE: NACA 65006 SYMMETRIC AIRFOIL PowerPoint PPT Presentation

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Title: EXAMPLE: NACA 65006 SYMMETRIC AIRFOIL


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EXAMPLE NACA 65-006 SYMMETRIC AIRFOIL
dcl/da 2p
cm,c/4 0
  • Bell X-1 used NACA 65-006 (6 thickness) as
    horizontal tail
  • Thin airfoil theory lift slope
  • dcl/da 2p rad-1 0.11 deg-1
  • Compare with data
  • At a -4º cl -0.45
  • At a 6º cl 0.65
  • dcl/da 0.11 deg-1
  • Thin airfoil theory
  • cm,c/4 0
  • Compare with data
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