iterative equation two unknown for parachute
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I need to calculate the radius of a recovery main parachute and I have two equation with two unknowns.
v=sqrt(2*Weight/(C_d*Rho*A)); % terminal velocity C_d-drag coefficient
r=sqrt((2*m*g)/(pi*C_d*Rho*velocity^2)); radius of the chute
As you can see, I need the terminal velocity to solve for radius and vice versa. I am a complete beginner at MATLAB and I have no idea how to compute it iteratively using MATLAB. Anyu help would be greatly appreciated. I tried sth myself and ofc it does not work. You can see it below.
%calculates the radius and terminal velocity of parachute during recovery
m=40; %mass of engine [kg]
g=9.81; % gravitational acceleration [m/s^2]
v=0; %terminal velocity [m/s]
C_d=1.2; % drag coefficient
Rho=1.229; % air density kg/m^3
Weight=m*g;
r=0; %radius of chute [m]
Drag= C_d*(Rho*v^2/2)*pi*r;
Drag=Weight; %at terminal velocity
A=3.2; %projected area of the chute [m^2]
tol= 0.05 %tolerance
while error <= tol
v_old=v;
r_old=r;
v=v+sqrt(2*Weight/(C_d*Rho*A));
r=r+sqrt((2*m*g)/(pi*C_d*Rho*velocity^2));
error=abs(v-1-v)
if error <= tol
break
end
end
1 commentaire
Suleyman Sahin
le 17 Août 2022
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