An endoreversible engine as in Section 1.7 is to be designed. It consists of the reversible Carnot engine and two heat exchangers serving the furnace and the cooler.
a) Prove that its power at maximum output can be written as
$$
I_{E, \text { mech }}=\frac{(h A)_f}{1+(h A)_f /(h A)_c} T\left[1-\sqrt{\frac{T_o}{T}}\right]^2
$$
where $f$ and $c$ refer to the furnace and the cooler, respectively.
b) If the power is maximized once more by dimensioning relative sizes of the heat exchangers optimally, we get
$$
I_{E, \text { mech }}=\frac{1}{4} h A \cdot T\left[1-\sqrt{\frac{T_o}{T}}\right]^2
$$
where $h A=(h A)_f+(h A)_c$ is the total transfer coefficient multiplying the difference of temperatures.
c) Show that the optimized power of such an engine increases proportionally to ( $\left.T-T_o\right) 2 / T$ for differences of temperatures which are not too large. This condition is quite applicable to today's range of temperatures. What does this mean for the designer of a power plant?