Can someone tell me why my graph isn't plotting?

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Kane Patrick Bobier
Kane Patrick Bobier el 23 de Oct. de 2020
Comentada: Star Strider el 23 de Oct. de 2020
I am trying to plot Coefficient of Drag (Cd) and Coefficient of Lift (Cl) vs. Angle of Attack (a). The code doesn't have any errors but nothing is boing plotted. My for loop produces the Cd and Cl values that I need. Can someone check my code?
%area
A = 0.152 * 0.3;
a = 0:5:50;
Pd = [
0.65,
0.65,
0.64,
0.59,
0.55,
0.53,
0.49,
0.43,
0.38,
0.33,
0.26
];
Fl = [
-17.23,
-4.6,
6.25,
13.37,
12.54,
13.82,
17.24,
19.51,
21.88,
22.83,
19.56
];
Fd = [
5.07,
5.41,
6.79,
10.23,
12.42,
16.46,
19.69,
23.38,
27.1,
30.02,
3.35
];
for i = 1:numel(Pd)
Cl = (Fl(i)/(Pd(i)*A))
Cd = (Fd(i)/(Pd(i)*A))
end
plot(a, Cl);
hold on;
grid on;
plot(a, Cd);
hold on;
grid on;
xlabel('a - Angle of Attack');
ylabel('Cl-(Coefficient of Lift) and Cd-(Coefficicent of Drag)');
title('Coefficients of Lift and Drag vs. Angle of Attack');

Respuesta aceptada

Star Strider
Star Strider el 23 de Oct. de 2020
Subscript ‘Cl’ and ‘Cd’ in the loop:
Cl(i) = (Fl(i)/(Pd(i)*A))
Cd(i) = (Fd(i)/(Pd(i)*A))
.
  2 comentarios
Kane Patrick Bobier
Kane Patrick Bobier el 23 de Oct. de 2020
Thank you! Works perfect.
Star Strider
Star Strider el 23 de Oct. de 2020
As always, my pleasure!

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