2.1. Cone Calorimeter Experimental Setup
We conducted combustion experiments using a cone calorimeter based on ISO 5660-1 to compare and analyze the pyrolysis and combustion characteristics of polymer fuels ABS and PVC. The cone calorimeter is an instrument that can quantitatively measure key thermal reaction characteristics, such as the HRR and mass loss rate (MLR), based on oxygen consumption calorimetry. It is widely used to obtain experimental data for modeling the pyrolysis of solid fuels[
7,
9].
For the experiment, 10-mm-thick ABS and PVC specimens were used to ensure thermally thick conditions. The specimens were fabricated as 100 mm × 100 mm squares having a heating area of 100 mm × 100 mm, and the edges were wrapped in aluminum foil to prevent deformation and damage. A metal mesh was attached to the top of the specimens to suppress shape changes and surface spalling caused by swelling during combustion.
Similar experimental conditions were set when comparing the pyrolysis characteristics of the two fuels. The heat flux was set to 50 kW/m², and radiant heat was applied vertically from the top of the specimens. The heat-flux value is appropriate for simulating the harsh conditions acting on walls or ceilings during the mid-to-late stages of an indoor fire, and it is commonly adopted in relevant standards and numerous studies[
10-
12]. The specimens were ignited by removing the standard pilot pin from ISO 5660-1 to induce self-ignition, with the aim of analyzing the spontaneous pyrolysis and combustion behavior under conditions without an external ignition source.
The combustion products generated during the experiment were removed through the exhaust system at the top of the hood, with the duct flow rate set at 24 L/s. These flow conditions provided a stable exhaust environment for measuring the oxygen concentration and combustion products and were applied identically in the numerical analysis (FDS).
The experiments for each condition were performed three times, and the effective heat of combustion (∆He), soot yield (Ysoot), CO yield (YCO), and residue fraction (νs) were calculated as the average values of the experimental results and used as FDS input values. The residue fraction was calculated by comparing the remaining mass after combustion with the initial mass and was incorporated into the FDS's solid pyrolysis model.
Figure 1(a) shows the appearance of the PVC specimen before combustion; a uniform gray surface indicates PVC’s pre-combustion state.
Figure 1(b) displays the pre-combustion state of the ABS specimens, which have the same shape and size but exhibit slight differences in terms of color and density of the surface.
Figure 1(c) depicts the experimental setup where the specimen is exposed to radiant heat within the cone calorimeter. The specimen is installed below the radiant panel, and the exhaust system is located above.
Figure 1(d) presents the surface condition of the PVC specimen after combustion. Extensive discoloration and non-uniform residues are observed, and some parts of the surface are rough and swollen, appearing puffed up.
Figure 1(e) shows the surface of the ABS specimen after combustion, with a thin residue remaining on some parts of the surface and exhibiting a relatively uniform shrinkage pattern. This indicates that ABS is a non-charring fuel; it does not form a thick carbonized layer after combustion and leaves only a small amount of carbonaceous residues. Meanwhile, the HRR and MLR measured in the experiment were used as criteria to validate the pyrolysis and combustion models by comparing them with the numerical analysis results.
Specifically, this experiment was a small-scale study conducted under fixed-oxygen-concentration (atmospheric conditions) and radiative-heat-transfer conditions in a cone calorimeter. Therefore, it did not reflect the effects of the convective heat transfer, oxygen concentration reduction, and complex thermal environments that occur in real large-space fires. Thus, the experimental results are intended for comparing fuel characteristics under these limited conditions, and the scope of interpretation must be considered.
2.2. Pyrolysis-Combustion Modeling and FDS Input Parameters
The FDS supports two methods for inputting combustion characteristics to numerically simulate the pyrolysis and combustion processes of solid fuels. The first method is to directly input the experimental heat release rate per unit area (HRRPUA); this involves a simple model that assumes a fixed pyrolysis reaction. The second is to use a pyrolysis model that is employed to dynamically calculate the heat and mass transfer phenomena occurring during combustion based on the material's physical properties and reaction parameters. We adopted the latter approach and precisely reproduced the pyrolysis and combustion processes based on the experimental characteristics of ABS and PVC fuels.
Energy conservation analysis was performed using the FDS's pyrolysis model, considering heat transfer at the solid fuel surface, mass release into the gas phase, external radiative and convective heat fluxes, and latent heat loss. As shown in
Figure 2, before ignition, external radiative heat (
q˙ext′′) and convective heat (
q˙conv′′) are supplied to the surface, and the net heat flux (
q˙rad′′) is determined based on the radiative losses from the surface (
q˙≠t′′), initiating the pyrolysis reaction. After ignition, flame radiative heat flux (
q˙flame′′) also acts on the surface, forming a positive feedback loop where the convective heat flux increases to promote pyrolysis and increase the rate of flammable vapor generation. Thus, changes in the thermal energy balance before and after ignition significantly affect the combustion sustainability and pyrolysis rate.
The temperature distribution within a solid fuel is expressed using the following one-dimensional heat conduction Eq. [13]:
where ρs,cp,s and ks denote the density, specific heat, and thermal conductivity of the solid fuel, respectively, and q˙s′′' is the heat source term due to radiative heat absorption or pyrolysis reactions. This equation is interpreted as a structure where the rate of temperature change with time inside a solid, ρscs∂Ts∂t, is altered by heat conduction flux and internal reactions. At the surface of the solid fuel, the following energy-conservation boundary condition is applied, and at the bottom of the solid fuel (y = M), an insulating material, such as low-density ceramic wool, is placed; thus, an adiabatic condition is applied as follows:
where q˙ext′′ is the radiant energy from surrounding flames or walls and calculated based on the view factor and radiosity solver. q˙flame′′ is the radiant energy generated from combustion products and soot, and the FDS calculates the spectrally averaged radiative properties using a discrete-object-based radiation solver. ∆Hv describes the heat balance, including the latent heat (endothermic heat) required for pyrolysis, and q˙rad′′ and q˙conv′′ are expressed as follows:
where q˙rad′′ is the radiative heat loss emitted from the surface to the outside, and according to the Stefan-Boltzmann law, ϵ is the surface emissivity and σ is the Stefan-Boltzmann constant. The surface convective heat flux, q˙conv′′, is generated from the temperature difference between the fuel surface and the surrounding gas and is determined based on the convective heat transfer coefficient, hc. In the FDS, this is calculated internally based on the flow conditions, with empirical formulas applied depending on whether the conditions are natural or forced. T∞ is the ambient gas temperature, and Ts is the solid surface temperature.
The MLR per unit area, m˙″, which occurs according to the pyrolysis reaction, is expressed using an Arrhenius-type equation and calculated by applying the following equation, considering the residue fraction, νs (solid residue volume fraction):
where As is the pre-exponential factor, Es is the activation energy, R is the gas constant, Ts is the fuel surface temperature, and ρ0 is the initial density. This equation is used to estimate the amount of volatile gases produced via pyrolysis. These parameters are adjusted based on experimentally obtained thermogravimetric (derivative thermogravimetric) curves and HRR results, and they are defined in the REAC and MATL blocks within the FDS input file.
The calculated MLR per unit area is multiplied with ∆He which is the effective heat released during combustion, to calculate the HRRPUA (Heat release rate per area), q˙″.
The FDS treats combustion reactions using the mixing-controlled method, based on the assumption that chemical reaction rates are infinitely high. Accordingly, combustion reaction equations are constructed based on the mixing ratio of fuel and air and the product yield. In this study, the combustion reaction equations for ABS and PVC are defined as follows[
14]:
Here, soot is modeled as a carbon-hydrogen composite particle, with a hydrogen mole fraction of XH = 0.1, and it is calculated as a molar mass as follows:
The formation coefficients of soot and CO are calculated from the following experiment-based equation:
where mF is the mass of 1 mole of fuel, mCO and mSoot are the molar masses of each product, and yCO and ySoot are the product yields obtained from cone calorimeter experiments, which were used to set up the combustion reaction equation.
To numerically simulate the pyrolysis and combustion characteristics of solid fuels, the FDS was utilized based on the energy-conservation equation described earlier.
Figure 3 depicts the analysis domain and grid configuration for simulating the cone calorimeter experimental conditions, with the same heat-flux conditions (50 kW/m²), fuel type (ABS and PVC), and ventilation flow rate (24 L/s) as those used in the experiment. The grid size was set to capture the fire characteristics adequately within the analysis domain, and the entire analysis domain was configured as 0.26 m × 0.26 m × 0.61 m. The grid size was set to 5.78 mm to adequately capture heat and soot behavior within the combustion zone. The appropriate grid resolution was evaluated based on the characteristic fire diameter (
D*), which represents the characteristic scale of a fire.
D* is defined as follows:
where
ρ∞,
cp, and
T∞ represent the density, specific heat, and temperature of the atmospheric state, respectively, and
g is acceleration due to gravity.
D* calculated based on Q̇ =7 kW (the HRR) is approximately 0.132 m. Applying a grid size (() of 5.78 mm results in a grid number ratio () of approximately 22.76. This is a high-resolution condition exceeding FDS's recommended resolution range (4-16), which is sufficient to ensure the accuracy of thermal and soot behavior analyses[
15,
16].
The thermophysical and pyrolysis properties of ABS and PVC under these conditions were compiled based on experimental results and previous studies and standardized to the FDS input format. Specifically, the residue fraction (
νs), effective heat of combustion (∆
Hv), soot yield (
ySoot), and CO yield (
yCO) were directly estimated from the ISO 5660-1 cone calorimeter experiments conducted in this study, whereas thermal properties such as the density (
ρs), specific heat (
cp,s), thermal conductivity (
ks), and Arrhenius coefficients (
As and
Es) were obtained from data reported in previous experimental studies[
14,
17]. The relevant key material properties are summarized in
Table 1.