Experimental analysis of a gyroid-based heat and mass exchanger for Maisotsenko cooling cycle

The increasing global demand for space cooling, driven primarily by climate change, highlights the need for sustainable alternatives to vapor-compression systems and dew-point evaporative cooling is emerging as a promising solution in this context, as it enables efficient air temperature reduction to levels lower than those achievable with conventional evaporative systems. This work presents a first experimental investigation of an innovative cross-flow heat and mass exchanger (HMX) based on gyroid triply periodic minimal surfaces applied to the Maisotsenko cycle, marking a shift from traditional parallel-plate paradigms by introducing a fundamentally different 3D heat and mass transfer topology that leverages complex geometric structures to enhance thermal performance. The device, manufactured in polylactic acid (PLA) through material extrusion, is characterized by a hydraulic diameter of 9.16 mm and has been tested at inlet air temperatures of 30 °C and 35 °C, with corresponding relative humidities of 43% and 32%, air velocities from 2.3 to 4.1 m/s and recirculation rates between 0.2 and 0.7. The HMX achieved a maximum temperature drop of 6.1 °C and a volumetric cooling capacity of 55.6 kW/m 3 , exceeding the typical values reported in literature for standard geometries. The maximum coefficient of performance (COP) of 9.1 was obtained at 35 °C, with r ≈ 0.2 and air velocity of ≈ 2.5 m/s. The results indicate that the turbulence-promoting nature of the gyroid geometry shifts the optimal operating range toward significantly lower air velocities (<2.5 m/s) compared to conventional planar HMX configurations, while higher velocities ( ≈ 4 m/s) lead to a rapid degradation of COP. Although the wet-bulb effectiveness was limited to slightly above 50% by both the conductive thermal resistance of PLA and the relatively short length of the HMX, the gyroid structure sustained intense mass transfer, maintaining outlet relative humidity above 83%, indicating an oversized wet channel and motivating geometrically asymmetric designs with longer dry channels and wider wet channels. • First experimental assessment of a gyroid-based TPMS heat exchanger for DPEC • Volumetric cooling capacity of 55.6 kW/m 3 exceeds standard HMX designs. • Maximum COP of 9.1 achieved at 35 °C with a 2.5 m/s characteristic velocity. • Outlet relative humidity above 83% confirms strong evaporation effectiveness. • Peak temperature drop of 6.1 °C was recorded at an inlet temperature of 35 °C.

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Publication Details

Journal
Applied Thermal Engineering
Published
2026-04-27
DOI
https://doi.org/10.1016/j.applthermaleng.2026.131197
Primary Topic
Advanced Thermodynamic Systems and Engines
Type
article
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article

Experimental analysis of a gyroid-based heat and mass exchanger for Maisotsenko cooling cycle

Marco Puglia, Nicolò Morselli, Giulio Allesina, Simone Pedrazzi et al.
Applied Thermal Engineering
Advanced Thermodynamic Systems and Engines
article

Experimental analysis of a gyroid-based heat and mass exchanger for Maisotsenko cooling cycle

Marco Puglia, Nicolò Morselli, Giulio Allesina, Simone Pedrazzi, Salvatore Cristiano
article en

Abstract

The increasing global demand for space cooling, driven primarily by climate change, highlights the need for sustainable alternatives to vapor-compression systems and dew-point evaporative cooling is emerging as a promising solution in this context, as it enables efficient air temperature reduction to levels lower than those achievable with conventional evaporative systems. This work presents a first experimental investigation of an innovative cross-flow heat and mass exchanger (HMX) based on gyroid triply periodic minimal surfaces applied to the Maisotsenko cycle, marking a shift from traditional parallel-plate paradigms by introducing a fundamentally different 3D heat and mass transfer topology that leverages complex geometric structures to enhance thermal performance. The device, manufactured in polylactic acid (PLA) through material extrusion, is characterized by a hydraulic diameter of 9.16 mm and has been tested at inlet air temperatures of 30 °C and 35 °C, with corresponding relative humidities of 43% and 32%, air velocities from 2.3 to 4.1 m/s and recirculation rates between 0.2 and 0.7. The HMX achieved a maximum temperature drop of 6.1 °C and a volumetric cooling capacity of 55.6 kW/m 3 , exceeding the typical values reported in literature for standard geometries. The maximum coefficient of performance (COP) of 9.1 was obtained at 35 °C, with r ≈ 0.2 and air velocity of ≈ 2.5 m/s. The results indicate that the turbulence-promoting nature of the gyroid geometry shifts the optimal operating range toward significantly lower air velocities (<2.5 m/s) compared to conventional planar HMX configurations, while higher velocities ( ≈ 4 m/s) lead to a rapid degradation of COP. Although the wet-bulb effectiveness was limited to slightly above 50% by both the conductive thermal resistance of PLA and the relatively short length of the HMX, the gyroid structure sustained intense mass transfer, maintaining outlet relative humidity above 83%, indicating an oversized wet channel and motivating geometrically asymmetric designs with longer dry channels and wider wet channels. • First experimental assessment of a gyroid-based TPMS heat exchanger for DPEC • Volumetric cooling capacity of 55.6 kW/m 3 exceeds standard HMX designs. • Maximum COP of 9.1 achieved at 35 °C with a 2.5 m/s characteristic velocity. • Outlet relative humidity above 83% confirms strong evaporation effectiveness. • Peak temperature drop of 6.1 °C was recorded at an inlet temperature of 35 °C.

Applied Thermal EngineeringVol. 299
University of Modena and Reggio Emilia (IT)
Affordable and clean energy
Openalex Percentile: Top 15%
Advanced Thermodynamic Systems and Engines
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