3.1. Experimental Behavior of Surface Fire Spread
Figure 2 shows the sequences of typical structures for spreading flames over a fuel bed with different wind velocities before the firebreak. For all conditions, the fire could spread steadily to the front of firebreak, and the fire spread behavior was basically similar for fixed wind velocity before the firebreak. As the wind velocity increased, the flame tilted from the burned to unburned fuel surface, even attaching to the fuel surface, and the flame length and flame volume obviously increased. Based on the previous work [
29,
30], the flame length is the distance from the center of the flame base to the flame tip and the flame angle is defined as the angle between the flame and the unburned surface. The flame length and flame angle during the surface fire spread were obtained by the side-view camera. The average values for a short period of time before the flame front reached the firebreak were used as the characteristic values of flame length and flame angle, as shown in
Figure 3. The variations of flame length and angle with time for a short period of time before the flame front reached the firebreak under wind conditions of 0 m/s, 1.5 m/s, and 3.0 m/s, marked with black, red and blue circles were also shown in
Figure 3. It can be seen that the flame angle and flame length do not vary much and fluctuate around a specific value over a period of time when the flame front reaches the firebreak. In addition, flame length increased with increasing wind velocity, while flame angle showed the opposite trend. As the wind velocity increased, the flame shifted from tilting towards the burned fuel to adhering to the unburned fuel ahead.
Figure 4 shows the variation of flame front with time as determined by the characteristic temperature of the thermocouples. The method of determining the position of the flame front of a surface fire by means of the characteristic temperature has also been used by previous work [
15,
30,
31]. It was found that the greater the wind velocity, the faster the flame front moved forward. Moreover, the flame front position showed an essentially linear variation with time, indicating a quasi-steady state during surface fire spread [
15,
17]. The rate of spread (ROS) of surface fire was obtained from the derivative of the flame front with time as shown in
Figure 5. The positions of the flame front at different moments during flame spread at wind velocity of 1.5 m/s, marked with circle were also plotted in
Figure 5. From
Figure 5, the ROS grows with increasing wind velocity and achieves the maximum value at wind velocity of 3 m/s.
3.2. Effectiveness of Firebreak
For different wind velocities and firebreak widths, different fire spread phenomena were observed after the firebreak, as shown in
Figure 6. The surface fire behaviors across the firebreak can be classified into three categories, that is, no ignition, ignition by flame contact and ignition by spot fires. When the wind velocity was low, the flame volume was relatively small, and consequently the firebreaks could successfully prevent the fuel surface after the firebreak from receiving sufficient heat to be ignited. As the wind velocity rose, the flame was elongated and tilted toward the fuel surface, and correspondingly the heat received by the unburned fuel after the firebreak enhanced, possibly resulting in the ignition of fuel after the firebreak by flame contact (marked with red box in
Figure 6). When the wind velocity was large enough, the burning fuel could be blown away along the fuel bed, similar to the behavior of spot fires, which ignite the fuel after the firebreak (marked with red circle in
Figure 6).
The ignition statistics of a surface fire across the firebreak are summarized in
Figure 7. When the wind velocity was not more than 1.0 m/s, the fuel after the firebreak could not be ignited for conditions with different firebreaks. As wind velocity changed from 1.5 m/s to 2.5 m/s, the surface fire could not successfully cross the firebreak for relatively larger firebreak conditions, but the fuel after the firebreak could be ignited by flame contact for relatively narrow firebreak conditions. When the wind velocity increased to 3.0 m/s, the burning fuel could be blown away along the fuel bed, and the fuel behind the firebreak was ignited by spot fire. In summary, the greater the wind velocity and the narrower the firebreak, the more likely the fuel behind the firebreak was to ignite successfully.
As analyzed previously, the surface fire experiments were investigated by introducing various wind velocities and firebreak widths, and identifying the different situations of not ignited, ignition by flame contact and ignition by spot fire crossing the firebreak. Subsequently, the effectiveness of the firebreak against surface fires was analyzed and compared in detail. According to previous work by Wilson [
25], the optimal firebreak is basically related to the fireline intensity I. Additionally, for the ignition conditions by direct contact flame, a simplified model to estimate a fire crossing a firebreak by the fireline intensity I (MW/m) was proposed by Frangieh et al. [
22], which can be expressed as follows:
where
is the firebreak width (m),
is the fire spread rate before the firebreak,
is the flame height, and
is the fuel load consumed by the fire.
Figure 8 shows the firebreak width as a function of fireline intensity I, which is compared with predicted results by Equation (1). It can be noted that the slope of the linear fit is larger in this paper compared with the results reported by Wilson [
25], which may be due to the differences in the experimental conditions, scale, and fuel between this experiment and Wilsons’ work.
3.3. Temperature of the Fuel
The temperature development of the fuel before and after the firebreak as a function of time for different ignited conditions with various wind velocities is shown in
Figure 9, respectively. For all the conditions, the fuel surface temperature before the firebreak increased rapidly to above the pyrolysis temperature, and then decreased gradually to ambient temperature as the fuel burned out. For not ignited conditions, a significant difference in fuel temperature before and after the firebreak was observed. The fuel temperature after the firebreak varied slightly and was much lower than the pyrolysis temperature of the fuel. However, for the ignited conditions, the fuel temperature increased to exceed the pyrolysis temperature of the fuel, and the fuel was ignited and the flame could continue to spread, which was obviously different from the unignited conditions.
Moreover, the variations of the fuel temperature after the firebreak were also different for different ignition conditions, as shown in
Figure 9b,c. In the cases of fuel ignited by contact flame, a slow rise in temperature of the fuel after the firebreak before a steep rise was observed, which characterizes the heat absorption process of the fuel before ignition. Nevertheless, only a steep rise in temperature of the fuel after the firebreak was found for ignition conditions by spot fire, where the burning fuel was blown across the firebreak and then ignited the fuel after the firebreak directly. Additionally, for ignition conditions by contact flame, the flame reached the position of each thermocouple in turn, including the thermocouple above the fuel after the firebreak. Whereas, due to the appearance of spot fires, the fuel behind the firebreak could be ignited in different positions, and the fuel temperature rise behind the firebreak may not have followed the same order. As shown in
Figure 9c, the temperature of the fuel at 10 cm behind the firebreak rose earlier than that of the fuel at 0 cm behind the firebreak.
The fuel surface temperature before and after the firebreak for not ignited conditions with various wind velocities is shown in
Figure 10, where the peak value of temperature is selected as the characteristic value. As can be seen from the figure, the fuel surface temperature increases as the wind velocity grows larger, due to the fact that flame length gets longer and the flame tilts toward the unburned fuel. Additionally, it can be noted that before the firebreak, the maximum temperature exceeded the pyrolysis temperature of the fuel, whereas after the firebreak, the maximum temperature dropped dramatically to below the pyrolysis temperature, and even the fuel temperature in some conditions was only about 40 °C. This observation indicates that the firebreak can effectively prevent the heat transfer from the flame to the unburned surface, and limit the temperature rise of the fuel after the firebreak. Moreover, for a fixed wind velocity, the wider the firebreak, the lower the fuel temperature after the firebreak, and it can decrease with an increase in distance. Additionally, as wind velocity increases, the fuel temperature after the firebreak accordingly increases, which is attributed to the enhanced heat flux from the flame front to the unburned fuel caused by the wind effects.
The typical temperature variations of the fuel after the firebreak as a function of time for ignited conditions are plotted in
Figure 11, in which the dotted line represents the moment the fuel after the firebreak is ignited. As can be seen from
Figure 11a, for the ignition conditions by contact flame, the fuel temperature exceeds 253 °C when the fuel after the firebreak is ignited. The greater the wind velocity, the faster the fuel after the firebreak will be ignited. The temperature of the thermocouple closest to the ignition location at the moment of ignition and the maximum temperature of this thermocouple are labeled in the
Figure 11b for the ignition conditions by spot fire. From the figure, the thermocouple closest to the ignition location initially does not reach the pyrolysis temperature of the fuel when the fuel after the firebreak is ignited at a certain position, and then gradually increases to the pyrolysis temperature. Also, in the case of ignition by spot fire, the heating of the thermocouples is non-sequential, i.e., the thermocouple closest to the ignition position probably heats up earlier than the thermocouples ahead of it.
The characteristic temperatures of the fuel after the firebreak for various wind velocity and firebreak conditions are summarized in
Figure 12. In this work, the maximum temperature of the first thermocouple behind the firebreak for the unignited cases is concluded in
Figure 12, and for the contact ignition cases the temperature at the moment of ignition of the first thermocouple behind the firebreak is compared in
Figure 12. Whereas, due to the random character of the spot fire, the temperature of the thermocouple closest to the ignition position at the moment of the ignition and the maximum temperature of this thermocouple are also summarized in
Figure 12. Obviously, for the unignited conditions, the fuel temperature after the firebreak was not more than 150 °C and was far less than the pyrolysis temperature of the fuel. As the wind velocity increased, the maximum temperature after the firebreak for unignited conditions increased correspondingly, which indicates that the flame and heat transfer are enhanced by the effects of wind. However, the temperature when the fuel ignited by flame contact and the maximum temperature for ignition conditions by spot fire are all greater than 253 °C. This critical temperature of 253 °C is basically close to the pyrolysis temperature of the fuel.
3.4. Heat Flux
The typical variations of heat flux, including total heat flux (
) and radiation heat flux (
) over time for different ignition conditions are plotted in
Figure 13a, which are obtained by the heat flux sensors. The values of heat fluxes were smoothed by FFT low-pass filtering, and this method was also applied by previous work [
14]. It can be seen that as the flame front approaches the heat flux sensor, the value of heat flux before the firebreak increases accordingly until it reaches the maximum value, and then gradually decrease. Moreover, greater total and radiation heat fluxes are observed with increasing wind velocity, which is attributed to the fact that the flame length is elongated and the flame tilts toward the unburned fuel under conditions of increasing wind velocity. It was found that when the flame fails to spread across the firebreak, the total heat flux and its growth rate after the firebreak were obviously less than that before the firebreak, and a similar variation was also observed in the radiation heat flux. But for the ignition conditions by contact flame, the difference between the growth rates of total and radiation heat fluxes before and after the firebreak was not significant. Due to the removal of the heat flux sensors after the firebreak when the fuel after the firebreak was ignited, the values of total heat flow after the firebreak did not increase to be similar to the region before the firebreak. As the wind velocity increased to 3.0 m/s, which was the ignition conditions by spot fire, the total and radiation heat fluxes both exceeded the range of the heat flux meter, which were not described and analyzed in detail in this work.
The heat flux before and after the firebreak for no ignition conditions with various wind velocities and firebreak widths is shown in
Figure 13b, in which the heat flux when the fire front reaches the heat flux meter is taken as the characteristic value. It can be observed that whether before or after the firebreak, both corresponding total and radiation heat fluxes increase significantly as the wind velocity rises, which also shows that the heat flux of the unburned fuel can be reinforced by the wind effects. This is attributed to the fact that when the wind is present, the flame length is elongated and the flame tilts toward or even attaches to the fuel surface, which consequently promote the heat transfer. Moreover, when the firebreak appears, the total and radiation heat flux received by the fuel surface after the firebreak significantly decreased, and decreased with the increase of the width of firebreak. Nevertheless, as the width of the firebreak increased, the decrease rate of heat flux received by the fuel surface after the firebreak became smaller.
In order to further investigate the effects of firebreak on radiation in the surface fire spread, a simplified model of radiation was analyzed and described. According to the previous observations in this work, the flame can be assumed to be a tilted plane with uniform temperature and emissivity. The radiation heat flux received by a micro-element on the centerline of the fuel bed can be estimated by the following formula [
15,
17]:
where
denotes the radiation heat flux received by the unburned surface,
and
are the flame temperature and ambient temperature, respectively, and
denotes the view factor between the flame front and the micro-element, which can be expressed as follows for a tilted plane flame [
8]:
where
is the distance between the flame base and the element,
is the width of the fuel bed,
is the flame length, which is the length from the flame tip to the flame base and
is the flame angle, which can be defined as the angle between the flame sheet and the fuel surface. The flame length and flame angle before the firebreak can be obtained from the video analyzed frame by frame in a relatively steady stage.
Figure 14 plots the view factor
as a function of firebreak width for various wind velocities. It can be found that as the firebreak width increased, the view factor
decreased significantly, but it showed an opposite trend with wind velocity. This variation is similar to the trend of the experimental results.
Many previous works have investigated the variation of heat flux during the spread of surface fires. For instance, Cohen et al. [
32] reported that a radiation heat flux of 31 kW/m
2 is the ignition limit of thermally thick wood. However, unlike the ignition of thick wood, the value is lower for vegetation ignition [
32]. Additionally, Frangieh et al. [
22] numerically studied the effectiveness of a fuelbreak on surface fire spread, and found that in wind driven cases, the heat transfer by convection and radiation both contribute to the ignition process. Mell et al. [
33] comparatively analyzed the effects of convection and radiation heat flux on fire spread by computational fluid dynamics (CFD) simulation of a fire spreading through an excelsior fuel bed in the absence of an ambient wind. In this work, heat transfer of radiation heat flux is analyzed and compared. However, the total heat flux received by the fuel surface after the fuel break was greater than the radiation, especially in conditions of greater wind velocities as compared in
Figure 13b, which also demonstrates the importance of convection in surface fire spread. Therefore, the characteristic total heat fluxes after the firebreak for various wind velocity and firebreak conditions are presented and compared in this work, as shown in
Figure 15, which shows the maximum total heat flux for the unignited condition and the total heat flux when the fuel ignited by flame contact, respectively. It can be noted that for the unignited condition, the maximum total heat flux after the firebreak is not more than 43 kW/m
2, while the total heat flux after the firebreak when the fuel ignited is greater than 43 kW/m
2 for ignition conditions by contact flame. In addition, for unignited conditions, the maximum total heat flux after the firebreak increases with the wind velocity, but shows an opposite trend with firebreak width.