The numerical analysis was performed in this study both specifically for the BIPVT system and for the integration of the BIPVT system into the test room façade. The numerical analysis was structured in three parts. The first part described and characterized the case study. The second part developed the whole-building dynamic simulation employing a parametric analysis. The third part developed the CFD simulation.
The heat balance of the BIPVT system is presented in
Figure 2. It considers the solar gains and conductive and convective heat fluxes throughout the module. The heat transfer through radiation within the system was ignored in this scheme. In this scheme,
qint stands for heat flux through the interior elements,
qpv for heat flux through the photovoltaic module,
qv for convective heat flux and G
D for direct solar radiation.
2.1. BIPVT Control Logic
The control strategies fundamentally contribute to achieving the NZEB concept. Among the different objectives of the control strategies, some of the most important are the comfort of the occupants and the efficiency of energy use while reducing the energy demand of a building. The control of the systems also has the potential to contribute to demand response strategies, as in [
12]. The smart scheduling of the operation of the systems is important not only in scenarios in which model predictive controls are employed to reduce energy use in the building itself, as in [
12,
26], but also in a more general context in which the actions of the building systems are a part of the grid energy flux planning.
In its current state, the BIPVT system installed in the test room is manually operated. With the aim of improving the operation of the system, which can be subjected to occupants’ perception of the environment and also the availability for operation, the current study aims to assess the control logic throughout the parametric analysis of different setpoints for the BIPVT vents opening and closing. The proposed EMS control logic assessment for the automation of the BIPVT system does not account for the energy consumed to its own operation. Indeed, its focus is the reduction of the energy needs of cooling and heating of the adjacent thermal zone (the test room).
The proposed control logic process for the automatic operation scheme is presented in
Figure 3. It takes into consideration: the maximum temperature of comfort (
) and the minimum temperature of comfort (
) between which the occupant is considered comfortable (comfort range temperature (
); the indoor temperature (
); and the air cavity temperature (
). The temperatures considered for the operation may be changed according to the occupants’ preferences, in terms of setpoint definition for the smart operation of the system. However, during the development of this work, the
range was assumed to be between 18 °C (
) and 25 °C (
). The average temperature of the air cavity temperature (
) also interfered with the operation of the vents, as it is possible to see in the scheme. It is important to highlight here that the temperatures considered for the air cavity considering the obtained experimental values refer to a punctual value translating the temperature in the sensor’s location, whereas the average temperature accounts for all the sensors located within the air cavity (vertical duct, inlet and outlet).
2.2. Whole-Building Dynamic Energy Simulations
Most studies on building heating and cooling load calculations are strongly based on computer simulations, due to the challenges posed by the many aspects involved in modelling the entire building. To evaluate the interaction between the system and the room, EnergyPlus software [
27] was used (version 8.6.0.) with the primary purpose of estimating thermal changes, lighting levels, heating and cooling, natural ventilation, water uses, photovoltaic systems, thermal comfort indices, and other variables. It can be adapted to different climates from weather archives with hourly data. As a result, a wide range of calculated data, such as interior temperatures, surface temperatures, heat flow through building components, interior heat gains, air exchange, energy use and others, are obtained.
The real conditions dynamic simulation is focused on the Solar XXI NZEB test room and energy systems tested as integrated façade solutions. Overall, the main façade is south oriented, as was demonstrated in the case study section. The time step set for the simulation was 20-time steps per hours, beginning on 1 January and ending on 31 December, accounting for 8760 h simulated for each case in same boundary conditions regarding weather conditions for the parametric analysis (based on the original weather file for Lisbon) and a modified weather file for the model under validation process. The daylight saving period was set from 30 March to 30 October. The HVAC template used for nominal energy needs calculation was 20 °C for the constant heating setpoint and 25 °C for the constant cooling setpoint, and the results were obtained through the utilization of an ideal loads system.
First, the model for experimental validation was developed (M1). The M1 was elaborated to compare its results with the data recorded by the experimental campaign carried out at the test room site to validate the inputs inserted in the program. To ensure that the results obtained by computer modelling effectively represent the thermal behavior of the building, it was essential that the simulation model was calibrated correctly [
28]. The model was validated as given by [
29,
30] for the performance criteria of the model validation. The usage pattern (occupancy, lighting and equipment) registered in the building for the considered days was inserted into the validation model. Moreover, observational measurements were taken to confirm the infiltration calculations. The temperature sensor used (series PT100) had a sampling interval of 1 min, and 60-min averages were calculated once the output of the simulation had hourly sampling. The sensor was located in the middle of the room, avoiding direct solar gains.
Table 1 presents the sensors’ specifications.
The weather file containing the Test Reference Year (TRY) values of the city of Lisbon was modified, with radiation, temperature data and relative humidity recorded by the experimental campaign. The modification of the weather file may be a tricky process, and the steps follow the approach described in detail in [
31]. The weather file was modified using the experimental data from January and February of 2018, and the remainder of the file was kept as the original. After the modification of the weather file, this study followed the simulation of the validation model.
Table 1.
Sensor specifications.
Table 1.
Sensor specifications.
Observable Variable | Sensor Brand/Model | Range | Accuracy |
---|
Room temperature | Omega/PT100 [32] | −70 to 500 °C | 0.03–0.07 |
Outdoor temperature | Omega/PT100 [32] | −70 to 500 °C | |
Global horizontal radiation | Kipp & Zonen CM6B 951765 [33] | 200 to 4000 nm | <0.2% |
Direct normal radiation (weather station) | Kipp & Zonen CHP1 100434 [34] | 200 to 4000 nm | <0.2% |
Direct normal radiation (wall of test room) | Kipp & Zonen CHP1 100434 [34] | 200 to 4000 nm | <0.2% |
Diffuse horizontal radiation | Kipp & Zonen CM6B 983431 [33] | 200 to 4000 nm | <0.2% |
Air infiltration | Testo 425 | 0 m/s to 20 m/s | 0.01 m/s |
Air cavity temperature | Omega/PT100 [32] | −70 to 500 °C | 0.03–0.07 |
PV module temperature | Omega/PT100 [32] | −70 to 500 °C | 0.03–0.07 |
The simulation parameters used for the validation model are described in this sub-section and were kept for all the models developed in EnergyPlus in the scope of this work. The main simulation parameters and objects, and the value/option are described in
Appendix A. The results obtained for the model using EnergyPlus software were compared with the temperature measurements made within the thermal zones in which the case study was performed. The root mean square error (RMSE) and mean bias error (MBE) were calculated and compared with the maximum allowable values for validation [
28]. To achieve a more accurate validation of the model, two periods were used—from 22 January 2018 to 28 January 2018 and from 15 February 2018 to 22 February 2018—accounting for a total of 14 days. After validating the model, the parametric analysis proceeded. The parametric analysis accounts with different geometries for all the models. The geometries were developed, through the OpenStudio plug-in in SketchUp for the test room with the BIPVT element (
Figure 4).
The parametric analysis aimed to recognize the impact of different parameters in the overall building performance. After validating the model (M1), the scenarios for the parametric analysis were set (M2 to M16), and the reference models were developed (M4). M4 was the model that effectively represented the building with the system as it is, considering geometry, air cavity thickness and air flow between zones obtained by experimental campaign. The reference model M4 was used for comparison with other models in which different strategies were inserted.
To simulate these models, all the inputs needed were added into the model on EnergyPlus and the weather file that contains the values of TRY (Test Reference Year weather data) of the city of Lisbon was used without any kind of modification (and thus different from what was previously used in the validation model).
A utilization pattern was also established for occupation and equipment for working hours from Monday to Friday, from 08:00 a.m. to 12:00 p.m. and from 13:00 a.m. to 17:00 p.m. Lighting was not considered in the simulations. When the blinds were completely opened, the daylight was sufficient to generate visual comfort of the occupants. The lighting system constituted a considerable internal thermal gain to the thermal zone—for comparative purposes, lighting was not considered as well in the set of scenarios in which the blinds were considered closed. It must be acknowledge, however, that as a real condition lighting may be needed in a situation where blinds are closed to achieve visual comfort for the occupants.
The total thermal gains were convective, radiant and latent gain in various proportions. Convective gains are instantaneous additions of heat to the thermal zone since the radiant gains are distributed on the surfaces of the zones where they are first absorbed and then released. Latent gains, in turn, need to be handled through ventilation and air conditioning [
27].
The established BIPVT system infiltration of 0.01 m3/s and in the room 1.32 air change per hour were considered as constants during the simulation period. It is important to highlight that the BIPVT system was equipped with vents that increase the airflow of the natural convection through forced convection, and, despite not being tested in the experimental campaign, they were considered in the numerical analysis through the assumption of different airflow rates. The windows were closed all the time.
The scenarios simulated in the parametric analysis have been studied in terms of five groups of parameters:
Window blind position (open or closed);
Air gap thickness (0.5, 0.1, 0.16, 0.20 m);
Zone mixing airflow (0.01, 0.02, 0.03 m3/s);
Number of PV panels (4, 3, 2, 1 panel);
Zone mixing setpoint for operation.
Table 2 presents the scenarios with the blinds open (except M2, that is presented as an exceptional comparison in the table because it corresponds to the BIPVT system without ventilation/air changes with the interior test room and with closed blinds) and accounts for 15 scenarios (14 with the blinds open and 1 with the blinds closed). The scenarios in
Table 2 are also simulated with the blinds closed. While M2 corresponds to the model with the blinds closed and without ventilation/air changes with the interior test room, M3 correspond to the same configuration with the blinds open. For the BIPVT, M4 (the reference case, as previously explained) corresponds to the M1 (validation model) geometry configuration, but simulated for the whole year and with fixed parameters of ventilation between BIPVT air cavity and test room, whereas M1 was simulated in a free-floating mode for the validation period only (January and February) and no results for energy needs for cooling and heating are presented. Model 4 is represented by an air cavity thickness of 0.16 m, with a zone mixing airflow of 0.01 m
3/s, four PV modules, and a fixed zone mixing scheduled from December to February.
2.3. CFD Simulation
Following the whole-building dynamic simulation analysis, an additional brief assessment was completed using computational fluid dynamics (CFD) analysis. The numerical characterization of the façade elements was developed using the CFD approach through the use of the software Ansys Fluent [
35]. It aimed to characterize the thermal behavior of the system in its fluid and solid parts through the analysis of temperature profile, air velocity and turbulence, taking into consideration the cross-section of the element in a bidimensional analysis. Although all three heat transfer modes were present in or around the multielement façade systems which form the object of the present study, this work will place emphasis namely on the conductive and convective heat transfer mechanism.
The equations that govern the fluid flow and heat transfer processes inside the air gap formed between the vertical façade solid elements are the equations of mass, momentum and energy conservation [
36]. The fundamentals of the CFD technique are widely discussed in the literature and will not be further described here, besides the basics concerning the simulation set-up used. However, a detailed description of the computational fluid dynamics method may be found in [
37]. For this kind of calculation, it is critical to select appropriate boundary conditions that best represent the system.
The general scheme of analysis is briefly explained here. It began by designing the systems’ geometry using the Ansys Design Modeler according to the data provided in the case study description. The next step was to determine the mesh to be used in the fluid and solid parts, followed by the setup of the simulation. The setup of the simulation was done through the consideration of general features (as equations, steady-state mode, among others), model definition, the boundary conditions of the system, reference values, the solution, and initialization configurations. In the solution tab, it was possible to set the methods and monitors to be displayed, the variables to be calculated, and the reporting variables. The model results were observed through the selected plots and graphs.
The thermal behavior of the system was studied in a steady-state simulation. The simulation setup is briefly described here. The turbulent motion, described by the Navier–Stokes equations and characterized as an irregular condition of the flow with random variation with time and space coordinates, has been considered using the k-ε model with standard wall functions. These equations are solved by the use of the Semi-Implicit Method for Pressure-Linked Equations (SIMPLE) algorithm, and are essentially a guess-and-correct procedure for the calculation of pressure on the staggered grid arrangement introduced above. The method is illustrated by considering the two-dimensional laminar steady flow equations in Cartesian coordinates.
The energy model was considered activated. The turbulent viscosity was computed by combining k and ε, while the constants assumed the default values of C1ε = 1.44, C2ε = 1.92, C3ε = 0.09, σk = 1.0, and σε = 1.3. The standard k-ε model was used to perform the calculations in the software. The simplest “complete models’’ of turbulence are the two-equation models in which the solution of two separate transport equations allows the turbulent velocity and length scales to be independently determined. The pressure–velocity coupling used the coupled mode, whereas the influence of buoyancy force caused by the different densities due to the heating process was considered by inducting the Boussinesq approximation model (Boussinesq hypowork). This method uses a starting guess for pressure and velocity to solve the corresponding velocities via momentum equations, followed by introduced correction factors until convergence [
37].
The standard k-ε model is a semi-empirical model based on model transport equations for the turbulence kinetic energy (k) and its dissipation rate (ε). The model transport equation for k was derived from the exact equation. In contrast, the model transport equation for ε was obtained using physical reasoning and bears little resemblance to its mathematical counterpart, according to the software theory guide. The Boussinesq approximation was based on the assumption that the components of the Re stress tensor are proportional to the mean velocity gradients, assuming that eddies behave like molecules, that turbulence is isotropic, and that there exists local equilibrium between stress and strain.
Thus, default residuals were used for continuity, x-momentum, y-momentum, energy, turbulence kinetic energy and the turbulence kinetic energy dissipation rate for checking the convergence of the solution. The more detailed numerical formulation may be found in the software theory reference guide.
Figure 5 presents the boundary conditions and the domains of the system.
All CFD problems are defined in terms of initial and boundary conditions, as has been deeply explored in [
37]. Flows inside a CFD solution domain are driven by the boundary conditions, and the most common cause of the rapid divergence of CFD simulations is an inappropriate selection of boundary conditions. It is essential that the user specifies these correctly and understands their role in the numerical algorithm. In transient problems the initial values of all the flow variables need to be specified at all solution points in the flow domain. However, this work assumed steady-state conditions. The boundary conditions considered in the scope of the CFD simulation of this work were the inlet, outlet, solid surfaces and prescribed pressure. The most accurate simulations can only be achieved by supplying the measured inlet values of turbulent kinetic energy k and dissipation rate ε. However, in most cases, such data were often not available, and default values were adopted.
In this CFD analysis, the PV module was considered to be a heat source surface for all the BIPVT systems, with an associated temperature. The temperatures assumed for the PV surface () at a given moment (steady-state condition) were based on the experimental campaign previously developed, as well as the interior module/wall temperature. The interior wall of the BIPVT system was assumed to have the same temperature as the room ( at the initial boundary condition. The inlet velocity was considered as the value registered in the experimental campaign for the system (instant observation through the use of a non-fixed anemometer), corresponding to 0.0098 m/s normal to the boundary. The inlet turbulent intensity fraction was 0.5, and the turbulent viscosity ratio was 10. The outlet had a backflow direction specification method as normal to the boundary, while the backflow pressure specification was the total pressure. Moreover, the was assumed to be the same as the at a given moment.
All the elements were simulated under the same conditions of the heat source and inlet velocity to obtain comparable values. This was contrary to the experimental campaign in which each one of the elements was evaluated at a different time period with different boundary conditions. The PV surface was considered at 55 °C (based on the experimental data for the particular day of the BIPVT system). The was also the same as the experimental campaign for the given day. The outlet boundary conditions may be used in conjunction with the inlet boundary conditions. The air properties were sourced from the software database. The water properties were also sourced from the software database. The solid properties were mentioned in the case study description, and no-slip and no-permeability hydrodynamic condition along X and Y directions were considered.
It is essential to highlight that the real system temperature presented more heat losses, since in the CFD simulation the upper and bottom surface of the air cavity were considered adiabatic due to the lack of control in the experimental campaign to determine the heat fluxes through these surfaces. By simplification, the mesh was considered uniform for all the models. Considering these remarks, the results obtained for each simulation are presented in the following section.