EXAMPLE: NACA 65006 SYMMETRIC AIRFOIL - PowerPoint PPT Presentation
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EXAMPLE: NACA 65006 SYMMETRIC AIRFOIL
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EXAMPLE: NACA 65-006 SYMMETRIC AIRFOIL. Bell X-1 used NACA 65-006 (6% thickness) ... Thin airfoil theory lift slope: dcl/da = 2p rad-1 = 0.11 deg-1. Compare with data ... – PowerPoint PPT presentation
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Title: EXAMPLE: NACA 65006 SYMMETRIC AIRFOIL
1
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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