Please solve with MATLAB Please wright code in a codelike fo

Please solve with MATLAB. Please wright code in a code-like format.

Airplane wings are made of composite materials. A simple 1-D analysis of the heat transfer through 5 layers of the wing results in the following system of linear equations. You know the temperatures on the outer surfaces: T_6 = 273 K, the resistance through each material: R_A = 0.1 K/W, R_B = 0.001 K/W, R_C = 0.07 K/W, R_D = 0.04 K/W and R_E = 0.3 K/W, and the heat transfer rate: q = 68.5 W. Determine the temperatures between each layer of material and the inner surface. q = (T, - T_2)/R_A q = (T_2 - T_3)/R_B q = (T_3 - T_4)/R_C q = (T_4 - T_5)/R_D q = (T_5 - T_6)/R_E

Solution

function values = heatExchange(t6)
    rA = 0.1;
    rB = 0.001;
    rC = 0.007;
    rD = 0.04;
    rE = 0.3;
    q = 68.5;
  
    t5 = q * rE + t6;
    t4 = q * rD + t5;
    t3 = q * rC + t4;
    t2 = q * rB + t3;
    t1 = q * rA + t2;
    values = [t1,t2,t3,t4,t5];
end

This is the only code that can be written using the information you provided.