“…Beyond these differences, the jet tip penetration, the spreading rate of the jet, the axial decay of the fuel and the local mixing state can be Table 2. Subset of the matrix of nominal operating conditions from the Schlieren campaign of Vera-Tudela et al 30 (Table 1 consistently captured to very good agreement with the experiment at all operating conditions. By extension, the aspects of jet self-similarity in the far-field that are captured in the experiments can also be observed in the CFD results and are therefore not shown.…”
Section: Validation Of the Numerical Setupmentioning
confidence: 61%
“…A detailed schematic as well as the descriptions of the internal compartments and design parameters of the injector and of the high pressure circuit can be found in. 30 Figure 1 shows a schematic of the system used for the seeding of acetone into the injection fluid. Methane coming from the high-pressure circuit is led to a junction followed by two needle valves which regulate the amount of seeded and unseeded gas that will be fed into the injector.…”
Section: Constant Volume Chamber and Gas Injectormentioning
confidence: 99%
“…This steady-state flow rate is attained earlier at higher P inj , because the needle lift is faster. 30 Figure 11(b) shows the temporal evolution of injected methane mass in the CVC, calculated again from the simulations. All mass flow rates at a given P inj collapse onto each other.…”
Section: The Effect Of Injection Variations On Macroscopic Jet Characteristicsmentioning
confidence: 99%
“…In all cases, the faster jet penetration is also accompanied by faster volumetric growth rate, as shown in Figure 12). The injector dynamics also play some role in propagation speed and volumetric growth: the needle lift is faster at higher P inj , while being rather insensitive to the P ch 30 However, they do not fundamentally alter the picture of the physics, which is conveyed by equations ( 6) and ( 8), which will be discussed next.…”
Section: The Effect Of Injection Variations On Macroscopic Jet Characteristicsmentioning
This work presents a joint experimental and numerical study of global characteristics and mixing behavior of underexpanded methane jets at high-pressure conditions in a Constant Volume Chamber. Injection pressures of 200, 250, and 300 bar and pressure ratios of 4, 5, 6, 8, and 10 at each of those pressures have been investigated. Tracer LIF with acetone as tracer has been applied to experimentally quantify the mixing of methane and quiescent air. In order to exploit the symmetry of the configuration, accompanying simulations have been carried out in Reynolds-Averaged Navier-Stokes framework with the k – w SST turbulence model and real-gas modelling based on the Soave-Redlich-Kwong Equation of State has been employed to account for high-pressure corrections in thermodynamic and caloric properties. The experiments confirm the hyperbolic decay of axial fuel concentration and the Gaussian shape of traverse concentration profiles in the self-similar region of the jets, while simulation results match well with experimentally determined fuel concentration fields. It is found that scaling laws proposed in literature for steady-state jet propagation can qualitatively interpret the effect of injection variations on jet tip penetration and volume. Increasing pressure ratio at fixed injection pressure leads to the formation of slightly richer jets, with slightly smaller mass percentage in the range of air-to-fuel ratios most favorable to autoignition. By contrast, increasing pressure ratio at fixed chamber pressure leads to virtually identical Probability Distribution Functions of local air-to-fuel ratios and the same is observed when employing a fixed pressure ratio at higher pressure levels.
“…Beyond these differences, the jet tip penetration, the spreading rate of the jet, the axial decay of the fuel and the local mixing state can be Table 2. Subset of the matrix of nominal operating conditions from the Schlieren campaign of Vera-Tudela et al 30 (Table 1 consistently captured to very good agreement with the experiment at all operating conditions. By extension, the aspects of jet self-similarity in the far-field that are captured in the experiments can also be observed in the CFD results and are therefore not shown.…”
Section: Validation Of the Numerical Setupmentioning
confidence: 61%
“…A detailed schematic as well as the descriptions of the internal compartments and design parameters of the injector and of the high pressure circuit can be found in. 30 Figure 1 shows a schematic of the system used for the seeding of acetone into the injection fluid. Methane coming from the high-pressure circuit is led to a junction followed by two needle valves which regulate the amount of seeded and unseeded gas that will be fed into the injector.…”
Section: Constant Volume Chamber and Gas Injectormentioning
confidence: 99%
“…This steady-state flow rate is attained earlier at higher P inj , because the needle lift is faster. 30 Figure 11(b) shows the temporal evolution of injected methane mass in the CVC, calculated again from the simulations. All mass flow rates at a given P inj collapse onto each other.…”
Section: The Effect Of Injection Variations On Macroscopic Jet Characteristicsmentioning
confidence: 99%
“…In all cases, the faster jet penetration is also accompanied by faster volumetric growth rate, as shown in Figure 12). The injector dynamics also play some role in propagation speed and volumetric growth: the needle lift is faster at higher P inj , while being rather insensitive to the P ch 30 However, they do not fundamentally alter the picture of the physics, which is conveyed by equations ( 6) and ( 8), which will be discussed next.…”
Section: The Effect Of Injection Variations On Macroscopic Jet Characteristicsmentioning
This work presents a joint experimental and numerical study of global characteristics and mixing behavior of underexpanded methane jets at high-pressure conditions in a Constant Volume Chamber. Injection pressures of 200, 250, and 300 bar and pressure ratios of 4, 5, 6, 8, and 10 at each of those pressures have been investigated. Tracer LIF with acetone as tracer has been applied to experimentally quantify the mixing of methane and quiescent air. In order to exploit the symmetry of the configuration, accompanying simulations have been carried out in Reynolds-Averaged Navier-Stokes framework with the k – w SST turbulence model and real-gas modelling based on the Soave-Redlich-Kwong Equation of State has been employed to account for high-pressure corrections in thermodynamic and caloric properties. The experiments confirm the hyperbolic decay of axial fuel concentration and the Gaussian shape of traverse concentration profiles in the self-similar region of the jets, while simulation results match well with experimentally determined fuel concentration fields. It is found that scaling laws proposed in literature for steady-state jet propagation can qualitatively interpret the effect of injection variations on jet tip penetration and volume. Increasing pressure ratio at fixed injection pressure leads to the formation of slightly richer jets, with slightly smaller mass percentage in the range of air-to-fuel ratios most favorable to autoignition. By contrast, increasing pressure ratio at fixed chamber pressure leads to virtually identical Probability Distribution Functions of local air-to-fuel ratios and the same is observed when employing a fixed pressure ratio at higher pressure levels.
“…The new test rig is intended to fill the gap among: (1) constant volume cells (which are not suitable for premixed or dual fuel combustion); (2) rapid compression and expansion machines (which are limited in operating pressure and the achievable in-cylinder flow fields/turbulence levels); Constant volume, high pressure and high temperature cells such as the HTDZ (high temperature and high pressure cell) [6][7][8][9], or the much larger SCC (spray combustion chamber) [10][11][12][13], are valuable tools to investigate fundamental processes related to diffusion combustion with liquid fuel or high-pressure gas jets [14]. Experiments with premixed or dual fuel combustion however are very difficult due to long residency time of the ignitable fuel air mixture at high temperatures (in electrically heated cells), or because the pre-combustion required to reach high gas temperatures consumes all fuel present in the cell before the actual experiment (i.e., liquid fuel injection/ignition).…”
A new test rig has been designed, built and commissioned, and is now jointly pursued to facilitate experimental investigations into advanced combustion processes (i.e., dual fuel, multi-mode) under turbulent conditions at high, engine-like temperature and pressure levels. Based on a standard diesel engine block, it offers much improved optical access to the in-cylinder processes due to its separated and rotated arrangement of the compression volume and combustion chamber, respectively. A fully variable pneumatic valve train and the appropriate preconditioning of the intake air allows it to represent a wide range of engine-like in-cylinder conditions regarding pressures, temperatures and turbulence levels. The modular design of the test rig facilitates easy optimizations of the combustion chamber/cylinder head design regarding different experimental requirements. The name of the new test rig, Flex-OeCoS, denotes its Flexibility regarding Optical engine Combustion diagnostics and/or the development of corresponding Sensing devices and applications. Measurements regarding in-cylinder gas pressures, temperatures and the flow field under typical operating conditions are presented to complete the description and assessment of the new test rig.
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