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// scilab Code Exa 11.7 flow and loading coefficients
u=339.29; // in m/s
cx=180; // Axial velocity in m/s
alpha_1m=25; // air angle at rotor and stator exit
phi(1)=0.2;
phi(2)=0.4;
phi(3)=cx/u;
phi(4)=0.6;
phi(5)=0.8;
n=5;
for i=1:n
shi(i)=1-phi(i)*(2*tand(alpha_1m));
disp(phi(i),"when flow coefficient phi=")
disp(shi(i),"then loading coefficient shi=")
end
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