The utilization of gas turbine exhaust
heat through a Heat Recovery Steam Generator (HRSG) is an important effort to
improve power plant efficiency while reducing CO2 emissions, in which the tube
arrangement of the superheater both transversal pitch (ST) and longitudinal
pitch (SL) significantly affects convective heat transfer effectiveness and
pressure drop in the gas flow. This study aims to analyze the influence of ST
and SL variations on the heat transfer and fluid flow characteristics of a
superheater in a Solar Mars 100 GN gas turbine-based HRSG, in order to
determine the configuration with the highest heat transfer rate combined with
the lowest pressure drop, using numerical simulation with Computational Fluid
Dynamics (CFD) based on ANSYS Fluent across nine combinations of ST and SL,
namely V1 (100,45 : 98,63 mm), V2 (100,45 : 123.63 mm), V3 (100,45 : 148,63
mm), V4 (125,45 : 98,63 mm), V5 (125,45 : 123,63 mm), V6 (125,45 : 148,63 mm),
V7 (150,45 : 98,63 mm), V8 (150,45 : 123,63 mm), and V9 (150,45 : 148,63 mm).
Heat transfer performance was evaluated using the Nusselt Number (NU), pressure
drop was represented by the Euler Number (EU), and overall performance was
analyzed using the Performance Evaluation Criterion (PEC). The results show
that decreasing ST and SL increases the Heat Transfer Rate, Heat Transfer
Coefficient, and Nu, with ST having a more dominant influence than SL, V1
produced the highest heat transfer performance while V9 produced the lowest,
whereas the lowest Eu was obtained at V7. Based on PEC evaluation, V1 achieved
the highest value of 210,75474 and V9 the lowest at 169,97855 a difference of
40,77619, or approximately 23,99%. Although V1 exhibits a relatively higher
pressure drop due to its tightest pitch spacing, the resulting increase in heat
transfer coefficient and NU compensates for this drawback, making V1 the
optimal tube configuration due to its balanced heat transfer effectiveness and
pressure drop.