*ARCHIVED* development moved to aircraft-studio.
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function z = get_z(,)
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if (<0)
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disp('invalid X')
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end
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M = 0.02;
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P = 0.4;
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T = 0.12;
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a0 = 0.2969;
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a1 = -0.126;
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a2 = -0.3516;
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a3 = 0.2843;
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a4 = -0.1015;
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if x <P
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z_camber = M/P^2*(2**-^2);
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else
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z_camber = (/(1-)^2)*(1-2*+2**-^2);
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end
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%z_camber = M/P^2*(2**-^2);
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z_thickness = (/0.2)*(*^.5+*+*^2+*^3+*^4);
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if u==1
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z = z_camber + z_thickness;
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else
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z = z_camber - z_thickness;
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end
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