Activity of occupants and shifting method activation to utilize reduce temperature at evening. The goal with the study was to ascertain the momentary precise cooling energy according to the provide water temperature (Tin), the return water temperature from the . cooling ceiling (Tout), the water mass flow for the duration of regeneration (m), along with the total energy supplied for the cooling ceiling through regeneration with the phase change material. Convective heat flux density, radiant heat flux density, along with the heat transfer coefficient (convective, radiant) at the ceiling surface were calculated. two. Components and Methods Inside the analyzed case, there was unsteady heat transfer (the temperature field varies with time), and its intensity was dependent around the ambient temperature. Momentary radiant heat flux density (qr) was defined as in Equation (1): qr = C0 -2 TP 4 – TS 4 , exactly where C0 –Stefan oltzmann continual, C0 = five.6710-8 W/(m2 K4); TP –temperature on the non-activated surfaces, [K]; TS –surface temperature of activated panels, [K]; and 1-2 —Apricitabine site emissivity sensitive view factor [37,38]: 1-2 = where 1, two –emissivity of the emitting surface and emissivity in the heat absorbing surface (for building supplies: 1, two = 0.9.95), [-]; A1 , A2 –field of the emitting surface plus the heat absorbing surface, [m2 ]; and 1-2 –view issue [-]. Whereas momentary convective heat flux density (qc) was calculated as follows [39,40]: qc = c ti – ts), exactly where c –convective heat transfer coefficient, [W/m2 K]; ti –air temperature in room, [ C]; and ts –surface temperature of thermally activated panels, [ C]. The convective heat transfer coefficient between the radiant ceiling as well as the test chamber (c) was determined with Equation (4) (heating) and (5) (cooling): W/m2 (3)1-1 1 A 1 1 – 2 A two W/m(1)1-.[-](two)Apraclonidine Cancer within a heating mode (Ra 105 ; 1010): 0.27GrPr) 4 Nu c = = L LW m2 K(4)inside a cooling mode (Ra 806 ; 1.509):Energies 2021, 14,4 ofNu 0.15Gr r) three c = = L L where L–characteristic dimension of radiant ceiling panel, [m]; a –thermal conductivity of air, [W/(m)]; Nu–Nusselt quantity, [-]; Ra–Rayleigh number, [-]; c Pr–Prandtl number, Pr = p p [-]; Gr–Grashof quantity, Gr =W m2 K(five)–thermal expansion g–gravitational acceleration, [m/s2 ]; –density of air, [kg/m3 ]; ts – ti –temperature distinction in between thermally activated surface and air, [K]; and -dynamic viscosity of air, [kg/(ms)]. Ceiling cooling power [41]: mw w w qc = A where mw –water mass flow rate, [kg/s]; Tw –difference in between provide and return water temperature, [K]; cw –specific heat capacity, [J/(kg)]; and A–area of thermally activated surface, [m]. Thermal activation of ceiling (Qw) was performed at evening (from “start” to “stop”) plus the power intake during regeneration (water side) was calculated as follows:cease . . ts -ti |L3 coefficient, [m/s2 ];[-];W/m(6)Qw =startqc dtWh/m(7)Characteristic equation of the cooling panel proposed by standard EN 14037 and EN 14240 [28]: qm = Km n W/m2 (8) where Km –constant of the characteristic equation, [-]; T –temperature distinction in the active surface, [K]; and n–exponent from the characteristic equation of the active surface, [-]. 2.1. Experimental Chamber The tests were conducted in an experimental chamber with dimensions 4.7 four.1 3.0 m (W L H), which provided a steady partition temperature. The walls have been insulated with expanded polystyrene (thickness: 0.1 m) with the following parameters: density = 30 kg/m3 , distinct heat capacity cp = 1.45 kJ/(kg), and thermal c.
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