Abstract
In the previous report, the theoretical basic intercooling cycle was analyzed both when neglecting the pressure loss in the intercooler, and when considering it.Furthermore, using an approximate calculation method, the authors analyzed the change in the thermodynamic performance when intercoolers are used in a simple gas turbine.Here the authors, using the same approximate calculation method and considering the pressure loss in each component, analyze the change in the thermodynamic performance when an intercooler is used in the regeneration-reheat gas turbine.Then performance characteristics of the simple gas turbine with an intercooler are calculated using a more precise method.The results there of are compared to those obtained with the approximate method.
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