Consider a shell of thickness (dr) and of radii ( r ) and the temperature of inner and outer surfaces of this shell be T, (T−dT).
dtdQ= rate of flow of heat through it=drkA[(T−dT)−T]=dr−KAdT=−4π(kr)2dTdT[∵A=4πr2] To measure the radial rate of heat flow, integration technique is used, since the area of the surface through which heat will flow is not constant.Then,(dtdQ)r1∫r2r21dr=−4πKT1∫T2dTdtdQ(r11−r21)=−4πK(T2−T1)dtdQ=(r2−r1)−4πk1r2(T2−T1)⇒dtdQ∝(r2−r1)(r1r2)