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B.2. Examples of breakthrough profiles 1 0.8 0.6 0.4 0.2 0 trial 14 trial 11 trial 9 0 20 40 60 Time (s) Figure B1. Breakthrough profiles representative of the velocity range covered in the study. Experiments are at inlet conditions described in Table S1. Average Reynolds number across MTZ: trial 14 = 7.5, trial 11 = 4.7, and trial 9 = 2.8 B.3. Heat effects Figure B2 illustrates the heat effects present in our system. At the exact same conditions as the matched experimental curve, the model was run under isothermal and adiabatic conditions. It is clear that the matched experiment is very near adiabatic conditions. This figure also illustrates how the 0.9 cutoff was determined for defining the MTZ zone. For an isothermal MTZ, 0.95 is the more common cutoff. However, since the adiabatic response is stretched compared to the isothermal one, the location is matched. In other words, a 0.9 cut-off for the adiabatic case provides a reasonable estimate for a 0.95 cut-off on the isothermal curve. Since heat effects are relatively constant in the range of experiments, the difference between the experimental and isothermal curve should also be relatively constant, which justifies using the 0.9 160 C/C0PDF Image | LIMITS OF SMALL SCALE PRESSURE SWING ADSORPTION
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