%TestLiftDragCoeff

aoa = [-400:2:400];
aoa = [0:2:300];
Re = 10000:1000:30000;
%for i = 1:length(aoa)
    [CL CD] = LiftDragCoeff(Re,aoa);
%end

figure
plot(aoa,CD,'-x');
xlabel('angle of attack (deg)');
ylabel('Coefficient');
legend('Drag Coeff');

figure
plot(aoa,CL,'-x');
xlabel('angle of attack (deg)');
ylabel('Coefficient');
legend('Lift Coeff');