n-Hexane injection into high-temperature and high-pressure environments
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In this study, the process of n-hexane spray formation was investigated under a wide range of environmental conditions. The main aim of this research was to determine whether the global and visual properties of n-hexane spray change when the back pressure exceeds the critical pressure of the injected liquid. For this purpose, the liquid length and the boundary profile between the spray and surrounding air obtained by high-speed imaging of the Mie scattering signal were used. A major advantage of this work is that besides measuring global spray parameters, it provides quantitative analysis of the visual properties of the spray images; thus, the image analysis is not limited to qualitative visual impression. The results obtained in this study showed no step change in liquid length in terms of exceeding the critical parameters. Although qualitatively the boundary between the injected liquid and the surrounding gas seemed to become smoother in high-pressure and high-temperature conditions, the qualitative analysis did not support this observation.
KeywordsInjection Rapid compression machine RCM Spray Supercritical mixing Mie scattering
List of symbols
Gas pressure at start of injection
Rapid compression machine
Start of injection
Gas temperature at start of injection
Temperature of injected liquid
Injection into environments of pressure and temperature exceeding fuel critical parameters in terms of hydrocarbon fuels has become of high interest very recently. However, the supercritical mixing has been studied previously in terms of injection of liquid propellants and oxidizers in rocket propulsion (Chehroudi et al. 2002; Schmidt et al. 2002; Zong and Yang 2006; Segal and Polikhov 2008; Roy and Segal 2010). In many studies, researchers working on this topic linked the change in mixing behaviour to approaching and exceeding critical parameters of the injected liquid (Mayer et al. 1998; Chehroudi et al. 2002; Oefelein 2006; Oschwald et al. 2006; Zong and Yang 2006; Segal and Polikhov 2008; Rachedi et al. 2010; Roy and Segal 2010).
Mayer et al. (1998), studying liquid propellant injection into high-pressure environments, observed a remarkable difference between spray formation at sub- and supercritical pressure. Chehroudi et al. (2002) noticed a lack of any visual detection of drops when the back pressure approached and exceeded the critical pressure of the injectant. They had a visual impression of the gaseous jet and noticed the inhibition of the transition into the full atomization regime. Both research teams Mayer et al. (1998) and Chehroudi et al. (2002) concluded that the observed difference in the visual impression of the jet was caused by the fact that the surface tension approaches zero when the fluid pressure approaches and exceeds the critical value.
Segal and Polikhov (2008) concluded that transitional and supercritical mixing can be observed when only the temperature or the pressure is higher than the critical value of the injected liquid. They emphasized, however, that this observation is valid only when the second parameter is not substantially lower than the critical parameter of the injected liquid.
Experiments made by Rachedi et al. (2010) for a swirl injector showed that the behaviour of a supercritical hydrocarbon jet and a supercritical CO2 jet was similar in most investigated aspects. Dahms et al. (2013) showed that the mixing behaviour of a hydrocarbon fuel (n-dodecane) changes when the temperature of the surrounding gas exceeds the fuel's critical temperature. They noticed that for higher temperatures, darker regions signifying light scatter and extinction by liquid were still present in some locations. However, the transition from liquid to gaseous state appeared to be much smoother than at the low-temperature condition. They stated that while the fuel vaporization rates increased because of higher gas temperature, total vaporization of the liquid could not explain the lack of ligaments or droplets observed for the 900 K condition.
Dahms and Oefelein (2013, 2015) suggested that exceeding supercritical parameters of the injected liquid may not be sufficient for the mixing transition. In their work (Dahms and Oefelein 2013), their calculations revealed that enthalpy of hot surrounding gases is not sufficient to heat up the gas–liquid interface to its critical temperature. They suggested that the transition between two-phase and single-phase interface dynamics is not necessarily induced by diminished surface tension forces alone (Dahms and Oefelein 2013). Instead of reaching the injectant critical parameters’ criterion, they proposed a criterion of a Knudsen number lower than 0.1 for supercritical mixing. They defined the Knudsen number as the ratio of two-fluid interface thickness to the mean free path. Their considerations were focused on multi-component fluids, where in most cases the surface tension cannot be neglected. In single-component liquids, the surface tension may be neglected when the critical pressure of the liquid is exceeded.
The other important issue is the fact that immediately after the injection, a part of the injected liquid mixes with the surrounding gas and the properties of the mixture become completely different. The same researchers in the same study (Dahms and Oefelein 2013) stated that mixtures of a mixture fraction below 0.5 can be described as an ideal gas and the effects of real fluid behaviour do not play a role. Nevertheless, one needs to take into account that the process of such a mixture formation may be affected by real fluid behaviour.
Dahms and Oefelein (2015) noticed that mixing depends on the distance from the outlet of the nozzle. They suggested that the association of the continuum regime, where statistical fluctuations are negligible, is only valid in the dilute-gas regime but not in the dense-fluid regime associated with high-pressure liquid injection processes (Dahms and Oefelein 2015). Most recently Crua et al. (2017) confirmed the occurrence of the transition from classical liquid–gas mixing to mixing where surface tension forces diminish at high-pressure and high-temperature conditions. They, however, noticed that the transition to diffusive mixing does not occur instantaneously, but after some time when the liquid structures are surrounded by the hot ambient gas. They proposed a phenomenological model based on critical properties of the injected liquid to predict the transition from classical liquid–gas mixing to diffusive mixing.
In our previous study on n-hexane spray auto-ignition and combustion (Kapusta et al. 2016), depending on the conditions, a different visual impression of the spray was noticed, even though all cases were within the range of subcritical mixing according to the model proposed by Crua et al. (2017). In their study, long-distance microscopy with backlight illumination was used, capable of resolving a single droplet, which makes their approach very accurate in terms of formulating a criterion for the mixing transition. However, there is still a question of what this criterion has to do with macroscopic observations, especially some of those which have led to conclusions on the mixing transition close to critical point parameters, while the criterion formulated by Crua et al. (2017) is far from a critical point.
Therefore, in this study, we provide macroscopic spray visualization using high-speed imaging of Mie scattering, which is a well-accepted method for global spray visualization (Chen et al. 2014; Sun et al. 2018). It needs to be emphasized that this study is not limited to qualitative analysis based on the visual impression of the sprays, but also provides quantitative analysis of the spray-gas boundary. Moreover, we combine these observations with a liquid length analysis, in order to verify any possible link between visual impression and global spray properties.
2 Experimental set-up
The compression ratio in this research was set to 9. The RCM piston stroke was 81 mm, while the cylinder bore was 80 mm. The piston speed was around 1 m/s (depending on the air pressure under the piston).
In this study, a Siemens VDO piezoelectric gasoline outwards opening pintle injector was used. The injector was of a standard design without an inside swirl. The maximum needle lift was 40 µm (Gavaises et al. 2006), and the static flow rate was 36 g/s (Warnecke et al. 2006). Detailed geometrical data of the injector are shown in Gavaises et al. (2006). The injector was located in centre of the RCM head (Fig. 1) in order to inject the fuel into the centre of the combustion chamber where the thermodynamic conditions are least affected by the walls and the airflow acts symmetrically on the spray.
The in-cylinder pressure was measured by an AVL GM11D piezoelectric pressure transducer and an AVL IndiCom 621 data acquisition system. The spray was observed using a LaVision HSS5 high-speed camera at a frame rate of 20,000 fps with a resolution of 384 × 304 pixels. In order to avoid signal attenuation leading to non-uniform spray visualization (Chen et al. 2014), instead of light-sheet imaging, a global illumination was applied. The sprays were illuminated through the window in the piston by an external source of light (two halogen lights—500 W each), and the back-scattered light was recorded by the camera using the same window and mirror (Fig. 1).
In this study, n-hexane was used to reproduce conditions from the work of Kapusta et al. (2016). According to Linstrom and Mallard (2001), critical point parameters of n-hexane are: 507.6 ± 0.5 K and 3.02 ± 0.04 MPa. In all cases, injection pressure was the same at 20 MPa. The liquid temperature was set to 293, 323, 343, 373 and 423 K. Ambient air was used as a working gas. The air pressure at the start of injection varied from 0.36 to 7.06 MPa, while the temperature ranged from 450 to 1100 K. Note that the air temperatures at start of injection (SOI) were calculated based on an assumption of a uniform temperature and a constant polytropic coefficient.
3 Results and discussion
The time-average liquid length (i.e. average liquid length of a developed spray) decreases with increased pressure and temperature. It might be speculated whether exceeding the critical pressure has a stronger effect on liquid length than exceeding the critical temperature. However, if the cases for constant fuel temperature are considered, then the change in liquid length appears to be gradual. This shall be associated with increased density of the air inside the chamber, which increases along with pressure and temperature with piston movement. As shown previously by other researchers, gas density is one of the crucial parameters in terms of spray development for cylindrical nozzles (Hiroyasu and Arai 1990; Siebers 1999; Dos Santos and Le Moyne 2011; Ghurri et al. 2012) as well as for hollow-cone injectors (Dong et al. 2013). Moreover, as shown in Fig. 5, there is no specific change in time-average liquid length around critical pressure or temperature, which could be associated with a sudden change in the mixing process.
Another factor which may affect the spray-gas boundary and shall be taken into account is the boundary representation by the raster image. When the differences between spray fragments penetrating for short and for long distances become smaller, the effects of pixel resolution become more important and may lead to blurring of the spray-gas boundary. This effect is magnified when the liquid length is shorter. Then, also the average boundary of the spray is represented by the smaller number of pixels (smaller circle). The observed blurred spray-gas boundary in turn may be misinterpreted and associated with the effect of diffusive mixing, as shown in Fig. 2.
The observation of the spray formed by n-hexane injected into various environments made in this study clearly showed that the spray changes significantly with an increase in back pressure and temperature of the surrounding gas. The major difference was related to liquid length. However, the boundary between the spray and the surroundings seemed to be smoother and more diffusive in higher-pressure and higher-temperature conditions.
In high-temperature environments, higher heat transfer and vaporization rate stop the spray fragments, which are moving faster, from penetrating much further;
Smaller differences between spray fragments penetrating for short and for long distances caused by a decreased maximum liquid length in high-pressure conditions may become more blurred due to pixel resolution effects. This phenomenon is additionally enhanced by the arrangements as studied here; where with a decreased liquid length, the boundary between gas and spray is also decreased and represented by a lower number of pixels;
Only one measurement considered here was slightly above the condition for transitional mixing formulated by other researchers for single-component hydrocarbon fuel.
In general, taking into account the quantitative results presented in this study and the findings of other researchers, it may be concluded that a change in mixing appearance with an increase in surrounding pressure and temperature in a supercritical regime is observed. However, it is not necessarily associated with real gas effects, but maybe caused by the images’ visual properties, most probably coupled with other factors like a high evaporation rate in high-temperature conditions.
This study was funded by the National Science Centre of Poland within the framework of the OPUS programme under Agreement UMO-2012/07/B/ST8/03632.
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