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DR-107
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12-7-2014
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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:
0.16/0.2*1800*(0.2969*SQRT(x/1800)+(-0.1260*(x/1800)+(-0.3516*(x/1800)^2)+(0.2843*(x/1800)^3)+(-0.1015*(x/1800)^4)))
Excel:
=0.16/0.2*100*(0.2969*SQRT(X/100)+(-0.126*(X/100)+(-0.3516*POWER(X/100,2))+(0.2843*POWER(X/100,3))+(-0.1015*POWER(X/100,4)))
“c”=“D1@Sketch1”=1800
“t”=0.16
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