Mark Santangelo - Experimental Aircraft Builder's Log

Marks KitLog


Date: 12-7-2014
Number of Hours: 2.00
Manual Reference: DR7-1-904 thru 907
Brief Description: NACA0016 airfoils at all WS

Modelled NACA0016 airfoils at all Wing Stations - equation-driven Spline curves SW: 0.16/0.21800(0.2969SQRT(x/1800)+(-0.1260(x/1800)+(-0.3516(x/1800)^2)+(0.2843(x/1800)^3)+(-0.1015(x/1800)^4))) Excel: =0.16/0.2100(0.2969SQRT(X/100)+(-0.126(X/100)+(-0.3516POWER(X/100,2))+(0.2843POWER(X/100,3))+(-0.1015POWER(X/100,4))) “c”=“D1@Sketch1”=1800 “t”=0.16

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