A mathematical model has been developed to describe the isothermal operation of a single anode‐separator‐cathode unit cell in a redox‐flow battery and has been applied to the NASA iron/chromium system. The model, based on porous electrode theory, incorporates redox kinetics, mass transfer, and ohmic effects as well as the parasitic hydrogen reaction which occurs in the chromium electrode. A numerical parameter study was carried out to predict cell performance to aid in the rational design, scale‐up, and operation of the flow battery. The calculations demonstrate: ( i ) an optimum electrode thickness and electrolyte flow rate exist; ( ii ) the amount of hydrogen evolved and, hence, cycle faradaic efficiency, can be affected by cell geometry, flow rate, and charging procedure; ( iii ) countercurrent flow results in enhanced cell performance over cocurrent flow; and ( iv ) elevated temperature operation enhances cell performance.
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Fedkiw et al. (1984) studied this question.
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