2007
DOI: 10.1016/j.jpowsour.2007.06.057
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A mathematical model of a tubular solid oxide fuel cell with specified combustion zone

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Cited by 23 publications
(6 citation statements)
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“…Here, a large amount of heat equal to about 1.55 times the power output of the fuel cell is transferred to the entering air. However, the excess air is needed to provide air‐cooling in SOFC, and excess air reduces the temperature gradient and makes the cell temperature more uniform .…”
Section: Resultsmentioning
confidence: 99%
“…Here, a large amount of heat equal to about 1.55 times the power output of the fuel cell is transferred to the entering air. However, the excess air is needed to provide air‐cooling in SOFC, and excess air reduces the temperature gradient and makes the cell temperature more uniform .…”
Section: Resultsmentioning
confidence: 99%
“…This improvement derives from the gas transport resistance mainly because one electrode is thicker than the other that is optimal. In general, the over potentials of ohmic have to be hindered due to its significant effect upon the potential loss of cells [117][118][119]. Specifically, the ionic conductivity that derives from ion conducting elements at reaction region must be enhanced for cell functionality improvement to generate ohmic [120].…”
Section: Sensitivity Analysis Of Micro-structures and Electrodes-electrolyte Thicknesses For An Efficient Triple Phase Boundary (Tpb)mentioning
confidence: 99%
“…A precise emissivity of SOFC cathodes is uncertain; therefore, an emissivity value consistent with the literature is used, ε tube = 0.8 [12,13]. Sensitivity analyses have revealed radiation heat transfer to be relatively insensitive to surface emissivities because all radiation exchange occurs within relatively small enclosures.…”
Section: Cfd Model Settingsmentioning
confidence: 99%
“…Inlet conditions and system parameters applicable to a 650 W stack were supplied by the SOFC developer and are summarized in Table 2. The amount of stoichiometric air, air , for this hexadecane fueled system is calculated using the following, air = ṅ O 2 24.5 ·ṅ C 16 H 34 system inlet (13) Ambient conditions of T amb = 20 • C and P amb = 83 kPa surround the system insulation. The thermal boundary imposed to the outer insulation surface surrounding the system is convective with h = 10 W m −2 K −1 .…”
Section: Simulation Input Parametersmentioning
confidence: 99%