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Using Mach Up: http://aero.go.usu.edu/mu5/ , wingspan should be between 7-9ft

Helpful Tutorial: https://www.youtube.com/watch?v=N_oEZmDqm_Q

Airfoils and results:
Justin Fangzhi Wang (Deactivated) - NACA 4412

Brielle Chenier - NACA 2415

Cindy Cai (Deactivated) - NACA 1410

Airfoil shape

Conditions & Geometry

Results

NACA 1410

  • 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

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