true airspeed of different level

How can I plot a graph using the m-file function ?

The true airspeed of an aircraft in straight and level flight is given by ? = Sqrt(2?? /????) where ? – true airspeed ? – aircraft mass ? – acceleration due to gravity ? – air density ? – wing surface area ?? – coefficient of lift

Which the mass is 1204, the acceleration of gravity is 9.81, the air density is 1.0587 and 0.8198, the wing surface area is 12.203 adn the coefficient of lift is 0.6 ≤ ?? ≤ 1.4.

[Star Strider]

Use the linspace function to create the ‘CL’ vector. The rest is straightforward.

Answer 1

[David Hill]

I am not sure if this is what you are looking for.

g=9.81;
d=[1.0587,.8198];
S=12.203;
m=1204;
cl=linspace(.6,1.4,20);
hold on
for p=d
    V=sqrt(2*m*g/p/S./cl);
    plot(cl,V)
end

[Star Strider]

It is not appropriate to provide complete code for homework problems.