A Numerical Investigation on the Effect of Hydrogen and Syngas Addition on the Ignition of JP-8 Surrogates

Author(s):  
Thomas Helma ◽  
S. K. Aggarwal

A numerical study is carried out investigating the effect of hydrogen and syngas addition on the ignition of two JP-8 surrogates, a two-component surrogate and a six-component surrogate. This six-component surrogate has previously been found to accurately simulate the smoke point, volatility, flame temperature profiles, and extinction limits of JP-8, while the two component surrogates has been shown to reproduce the flame structure predicted with the six-component surrogate. CHEMKIN 10101 is used to simulate ignition in a closed homogenous reactor under adiabatic and isobaric conditions. The parameters include temperature ranging from 850–1250 K, pressure of 20 atm, and equivalence ratio ϕ = 1.0. The CRECK-0810 kinetic mechanism, involving 341 species and 9173 reactions, is used to model the ignition chemistry. For the conditions studied, the addition of H2 or syngas in small quantities has no effect on the ignition behavior of either the surrogates or their individual components. Addition of H2 or syngas in larger quantities increases and decreases the ignition delay at low and high temperatures, respectively. For the conditions investigated, the ignition behavior of both the surrogates is predominantly determined by the ignition chemistry of n-dodecane.

Author(s):  
Christopher Depcik ◽  
Michael Mangus ◽  
Colter Ragone

In this first paper, the authors undertake a review of the literature in the field of ozone-assisted combustion in order to summarize literature findings. The use of a detailed n-heptane combustion model including ozone kinetics helps analyze these earlier results and leads into experimentation within the authors' laboratory using a single-cylinder, direct-injection compression ignition engine, briefly discussed here and in more depth in a following paper. The literature and kinetic modeling outcomes indicate that the addition of ozone leads to a decrease in ignition delay, both in comparison to no added ozone and with a decreasing equivalence ratio. This ignition delay decrease as the mixture leans is counter to the traditional increase in ignition delay with decreasing equivalence ratio. Moreover, the inclusion of ozone results in slightly higher temperatures in the cylinder due to ozone decomposition, augmented production of nitrogen oxides, and reduction in particulate matter through radial atomic oxygen chemistry. Of additional importance, acetylene levels decrease but carbon monoxide emissions are found to both increase and decrease as a function of equivalence ratio. This work illustrates that, beyond a certain level of assistance (approximately 20 ppm for the compression ratio of the authors' engine), adding more ozone has a negligible influence on combustion and emissions. This occurs because the introduction of O3 into the intake causes a temperature-limited equilibrium set of reactions via the atomic oxygen radical produced.


2013 ◽  
Vol 17 (4) ◽  
pp. 1207-1219 ◽  
Author(s):  
Zouhair Riahi ◽  
Ali Mergheni ◽  
Jean-Charles Sautet ◽  
Ben Nasrallah

The practical combustion systems such as combustion furnaces, gas turbine, engines, etc. employ non-premixed combustion due to its better flame stability, safety, and wide operating range as compared to premixed combustion. The present numerical study characterizes the turbulent flame of methane-air in a coaxial burner in order to determine the effect of airflow on the distribution of temperature, on gas consumption and on the emission of NOx. The results in this study are obtained by simulation on FLUENT code. The results demonstrate the influence of different parameters on the flame structure, temperature distribution and gas emissions, such as turbulence, fuel jet velocity, air jet velocity, equivalence ratio and mixture fraction. The lift-off height for a fixed fuel jet velocity is observed to increase monotonically with air jet velocity. Temperature and NOx emission decrease of important values with the equivalence ratio, it is maximum about the unity.


Author(s):  
Michael V. Johnson ◽  
S. Scott Goldsborough ◽  
Timothy A. Smith ◽  
Steven S. McConnell

Continued interest in kinetically-modulated combustion regimes, such as HCCI and PCCI, poses a significant challenge in controlling the ignition timing due to the lack of direct control of combustion phasing hardware available in traditional SI and CI engines. Chemical kinetic mechanisms, validated based on fundamental data from experiments like rapid compression machines and shock tubes, offer reasonably accurate predictions of ignition timing; however utilizing these requires high computational cost making them impractical for use in engine control schemes. Empirically-derived correlations offer faster control, but are generally not valid beyond the narrow range of conditions over which they were derived. This study discusses initial work in the development of an ignition correlation based on a detailed chemical kinetic mechanism for three component gasoline surrogate, composed of n-heptane, iso-octane and toluene, or toluene reference fuel (TRF). Simulations are conducted over a wide range of conditions including temperature, pressure, equivalence ratio and dilution for a range of tri-component blends in order to produce ignition delay time and investigate trends in ignition as pressure, equivalence ratio, temperature and fuel reactivity are varied. A modified, Arrhenius-based power law formulation will be used in a future study to fit the computed ignition delay times.


Author(s):  
Young Chan Lim ◽  
Hyun Kyu Suh

Numerical study on the combustion chemical reaction of biodiesel fuel for the improvement of compression ignition combustion performance was studied in this work. The constant volume closed homogeneous reactor model was applied, at the same time, analysis conditions were set to 700∼900K of ambient temperature, and 15atm of ambient pressure. Also, the equivalence ratio was changed from 0.5 to 1.4 under the various mixing ratio, respectively. The results of analysis were compared in terms of ignition delay, combustion temperature, combustion pressure, NOx and CO emissions. Also, the total mass and the mass densities of the reactants were compared in the constant volume chamber. It was revealed that the value of ignition delay became shorter and combustion temperature and pressure were increased under the rich combustion conditions (Φ > 1.0). Furthermore, the CO emission was decreased under the lean combustion conditions (1.0 > Φ). Maximum value of NOx emission was observed when the equivalence ratio was 0.8 condition since the nitrogen and oxygen chemical reactions became actively than other cases.


2021 ◽  
Vol 898 (1) ◽  
pp. 012006
Author(s):  
Conghao Li ◽  
Jingfu Wang ◽  
Ying Chen ◽  
Xiaolei Zhang

Abstract Ammonia, as a carbon-neutral fuel, draws people attentions recently. NH3/CH4 blends is considered as a kind of fuel. A numerical simulation of the effects of CO2 dilution on the combustion characteristics and NO emission of NH3/CH4 counterflow diffusion flame was conducted in this study. Diffusion flame structure, the influence of CO2 radiation characteristics on temperature and NO emission characteristics were studies at normal temperature and pressure. The dilution and radiation of CO2 reduce the flame temperature significantly. NO concentration decreased with the CO2 mole fraction increase effectively. The study extends the basic combustion characteristics of NH3 containing fuel.


Author(s):  
Liang Feng ◽  
Zhongliang Liu ◽  
Yanxia Li

A numerical study on CH4 and air premixed combustion inside a small tube with a temperature gradient was undertaken to investigate the effects of inlet velocity, equivalence ratio and combustor size. The simulation results show that the inlet velocity has a significant influence on the reaction zone, and the flame front shifts downstream as the inlet velocity increases. The results also show that, the inlet velocity has no obvious effects on the flame temperature. The highest flame temperature is obtained if the equivalence ratio is set to 1. It is disclosed that the combustor size has a very strong effect on combustion characteristics. The smaller the combustor size is, the more difficult it is to maintain the steady combustion. The smallest combustor size that the stable flame can be sustained is determined mainly by the wall temperature of the microcombustor under the given conditions, and the higher the wall temperature is, the smaller the smallest combustor size. Therefore raising wall temperature is an effective way to realize flame stabilization for a given combustor size.


2015 ◽  
Author(s):  
Baolu Shi ◽  
Jie Hu ◽  
Satoru Ishizuka ◽  
Junwei Li ◽  
Ningfei Wang

To promote energy and environment security through combustion efficiency improvement as well as CO2 capture and sequestration (CCS), in this study oxygen enhanced combustion of methane has been investigated by using an inherently safe technique of rapidly mixed tubular flame combustion. As a new type of flame, the tubular flame has excellent flame characteristics such as negligible heat loss, aerodynamic stability and thermodynamic stability. Various applications have been proposed and demonstrated for determining the flammability limits, stabilizing a flame in a high speed flow, and obtaining a uniform and large-area laminar flame to heat iron slab or to reduce steel sheet surface. Especially, by individually injecting the fuel and the oxidizer into a cylindrical burner through four tangential slits hence, hence without flame flashback, the rapidly mixed tubular flame burner has been applied to analyze the characteristics of oxygen enhanced methane flame. To make a fundamental investigation, methane oxygen combustion has been attempted under various oxygen mole fractions with nitrogen and carbon dioxide as the diluents respectively. At first, nitrogen was added to the oxygen stream, and the oxygen mole fraction in the oxidizer was increased from 0.21 to 1.0. A stable, laminar tubular flame can be obtained from lean to rich when the oxygen mole fraction is no more than 0.4. And the maximum adiabatic flame temperature reaches around 2700 K. To enhance the mixing of fuel and oxidizer, nitrogen was also added to the fuel inlet to increase the injection velocity of fuel stream. The results show that by assigning the nitrogen to both the fuel and oxygen inlets to approach the same injection velocity, the flames become more uniform and stable. However, the range of stable tubular flame in equivalence ratio remains almost the same. Secondly, instead of nitrogen, carbon dioxide was used to dilute the methane/oxygen flames. Thus, the NOX emissions introduced by nitrogen will be greatly reduced, in addition, the main exhaust will be carbon dioxide and steam, which is beneficial for CCS. When carbon dioxide was only added into the oxygen stream, a stable tubular flame was obtained from 0.9 to 1.2 in equivalence ratio at the oxygen mole fraction of 0.21. With an increase of oxygen mole fraction, the stable tubular flame range enlarges in equivalence ratio, and up to the oxygen mole fraction of 0.50, stable tubular combustion could be achieved from lean to rich. By adding carbon dioxide to both the fuel and oxygen inlets to approach the same injection velocity, the upper limit of stable tubular flame increases much. Up to the oxygen mole fraction of 0.86, the stable combustion can be achieved at the stoichiometry, which gives a flame temperature around 3000 K. To fully understand the flame characteristics above, the chemical effects of carbon dioxide are numerical analyzed in comparing with the nitrogen diluted flames using the CHEMKIN PREMIX code with the GRI kinetic mechanism.


Fuel ◽  
2015 ◽  
Vol 158 ◽  
pp. 957-967 ◽  
Author(s):  
Raúl Payri ◽  
Juan Pablo Viera ◽  
Yuanjiang Pei ◽  
Sibendu Som

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