A composite wall has three different layers of material. Use the photo for reference. There is heat generation in Layer II where Gamma$($x$)=$ Gamma$\_$o$*($x$^2).$ The origin of x$=0$ will be in the middle of Layer II or the middle of Lb$.$ Reference the photo for all info needed. $1)$ Find Gamma$\_$o as a function of La$,$ Lb$,$ Lc$,$ k$1,$ k$3,$ T$1,$ T$2,$ T$\_$inf, h$,$ W$,$ H $[$HINT: Since T$1$ and T$2$ are known, you can find Q$].2)$ Find k$2$