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Airfoil shape

Conditions & Geometry

Results

NACA 1410

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  • velocity: 10ft/s

  • density: 0.093 slugs/ft^3 (styrofoam)

  • angle of attack: 0 (in air gliding)

  • geometry:

    • 5° mount angle, 3° washout, 10° sweep, 2° dihedral

    • root chord 1.5, tip chord 0.5

NACA 1410

^same as above except angle of attack: 15 degrees (lift-off??)

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