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Helpful Tutorial: https://www.youtube.com/watch?v=N_oEZmDqm_Q
Airfoil Data: http://airfoiltools.com/search/index?m%5Bgrp%5D=naca4d&m%5Bsort%5D=1
Terms:
CD - drag coefficient
CL - lift coefficient
Airfoils and results:
Justin Fangzhi Wang (Deactivated) - NACA 4412
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Airfoil shape | Conditions & Geometry | Results |
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NACA 1410 |
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NACA 1410 | ^same as above except angle of attack: 15 degrees (lift-off??) | |
NACA 2415 |
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NACA 0006 |
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NACA 4415 |
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