This document describes an experimental study of syngas combustion at elevated temperatures and the effect of adding water. Laminar flame speeds of syngas/air mixtures were measured over a range of fuel compositions, equivalence ratios, and preheat temperatures. The measured flame speeds were compared to simulations from existing chemical kinetic models, showing reasonable agreement at room temperature but large discrepancies at higher temperatures. Water was added to two syngas fuels up to 40% by volume, and different effects on flame speed were observed depending on the fuel composition and water concentration, related to competing chemical and physical impacts of water addition.
International Journal of Engineering Research and Development (IJERD)IJERD Editor
International Journal of Engineering Research and Development is an international premier peer reviewed open access engineering and technology journal promoting the discovery, innovation, advancement and dissemination of basic and transitional knowledge in engineering, technology and related disciplines.
Exergetic efficiency analysis of hydrogen–air detonation in pulse detonation ...BBIT Kolkata
Exergy losses during the combustion process, heat transfer, and fuel utilization play a vital role in the analysis of the
exergetic efficiency of combustion process. Detonation is thermodynamically more efficient than deflagration mode of
combustion. Detonation combustion technology inside the pulse detonation engine using hydrogen as a fuel is energetic
propulsion system for next generation. In this study, the main objective of this work is to quantify the exergetic efficiency
of hydrogen–air combustion for deflagration and detonation combustion process. Further detonation parameters are
calculated using 0.25, 0.35, and 0.55 of H2 mass concentrations in the combustion process. The simulations have been
performed for converging the solution using commercial computational fluid dynamics package Ansys Fluent solver. The
details of combustion physics in chemical reacting flows of hydrogen–air mixture in two control volumes were simulated
using species transport model with eddy dissipation turbulence chemistry interaction. From these simulations it was
observed that exergy loss in the deflagration combustion process is higher in comparison to the detonation combustion
process. The major observation was that pilot fuel economy for the two combustion processes and augmentation of
exergetic efficiencies are better in the detonation combustion process. The maximum exergetic efficiency of 55.12%,
53.19%, and 23.43% from deflagration combustion process and from detonation combustion process, 67.55%, 57.49%,
and 24.89%, are obtained from aforesaid H2 mass fraction. It was also found that for lesser fuel mass fraction higher
exergetic efficiency was observed.
MODELLING FOR CROSS IGNITION TIME OF A TURBULENT COLD MIXTURE IN A MULTI BURN...ijcsa
This document presents a computational model for determining the cross-ignition time of a turbulent cold mixture in a multi-burner combustor. The model accounts for various parameters that influence heat transfer during the cross-ignition process. Experimental validation was conducted using a simple test rig with two burners. Preliminary results from the experiments show relationships between cross-ignition time and factors like the flow area between burners, distance between burners, and flame properties. Computational fluid dynamics simulations will also be used to further investigate heat transfer in high-velocity regions and validate the model under more conditions.
The understanding of gas geochemical model to reduce the exploration uncertaintyRizal Abiyudo
The various fumaroles areas in the prospect are can be modelled by boiling depletion model and the relation between each of fumaroles. Geothermal waters would boil to create a first set of fumaroles and then the boiled, gas-depleted water outflows to the site of a second set of fumaroles where it boils again, creating fumaroles with gas-depleted chemistry.
EXPERIMENTAL INVESTIGATION ON THERMAL PERFORMANCE OF POROUS RADIANT BURNER AN...BIBHUTI BHUSAN SAMANTARAY
This paper presents the heat transfer characteristics of a
self-aspirating porous radiant burner (SAPRB) that operates
on the basis of an effective energy conversion method between
flowing gas enthalpy and thermal radiation. The temperature
field at various flame zones was measured experimentally by
the help of both FLUKE IR camera and K-type thermocouples.
The experimental setup consisted of a two layered domestic
cooking burner, a flexible test stand attached with six K-type
thermocouples at different positions, IR camera, LPG setup
and a hot wire anemometer. The two layered SAPRB consisted
of a combustion zone and a preheating zone. Combustion zone
was formed with high porosity, highly radiating porous
matrix, and the preheating zone consisted of low porosity
matrix. Time dependent temperature history from
thermocouples at various flame zones were acquired by using
a data acquisition system and the temperature profiles were
analyzed in the ZAILA application software environments. In
the other hand the IR graphs were captured by FLUKE IR
camera and the thermographs were analyzed in the
SMARTView software environments. The experimental results
revealed that the homogeneous porous media, in addition to
its convective heat exchange with the gas, might absorb, emit,
and scatter thermal radiation. The rate of heat transfer was
more at the center of the burner where a combined effect of
both convection & radiation might be realized. The maximum
thermal efficiency was found to be 64% which was having a
good agreement with the previous data in the open literature.
Optimizing Bunsen burner Performance Using CFD AnalysisIJMER
International Journal of Modern Engineering Research (IJMER) is Peer reviewed, online Journal. It serves as an international archival forum of scholarly research related to engineering and science education.
Effect of Ambient Temperature and Composition on Liquid Droplet CombustionIJERA Editor
An unsteady, spherically symmetric, single component, diffusion controlled gas phase droplet combustion
model was developed assuming infinite kinetics and no radiation effects. Finite difference technique was used to
solve time dependent equations of energy and species. Adiabatic flame temperature which is important for
calculating thermodynamic properties was calculated by employing a detailed method. Effects of ambient
temperature and composition on important combustion parameters like adiabatic flame temperature, droplet
mass burning rate, burning constant and droplet lifetime were obtained. Results indicated that flame
temperature, burning constant and mass burning rate increased with an increase in ambient temperature while
the droplet life time decreased. The present gas phase code was used in conjunction with the Olikara and
Borman code for obtaining concentration of important species. Emission results showed that for a 100m nheptane
droplet burning in standard atmosphere, an increase in ambient temperature led to an increase in NO
and CO concentrations and a decrease in CO2 and H2O concentrations. Extinction diameter for a 3000m nheptane
droplet burning in oxygen-helium environment was determined. Also, effects of ambient temperature
and composition were obtained on droplet lifetime and mass burning rate as a function of initial droplet
diameter. The present gas phase model is simple but realistic and can be incorporated in spray combustion
codes.
This document presents a theoretical analysis of the performance of a vapor compression refrigeration system using different refrigerants: R-12, R134a, and R1234yf. The analysis uses a computational model based on the first law of thermodynamics to investigate the effects of evaporating temperature, subcooling, condenser temperature, and liquid-vapor heat exchanger effectiveness on the system's coefficient of performance and refrigerating capacity. The results show that R1234yf has the highest relative capacity increase with increased subcooling and the highest percentage increase in COP. R134a requires the most compressor work. R1234yf is identified as a promising alternative to R134a due to its low global warming potential
International Journal of Engineering Research and Development (IJERD)IJERD Editor
International Journal of Engineering Research and Development is an international premier peer reviewed open access engineering and technology journal promoting the discovery, innovation, advancement and dissemination of basic and transitional knowledge in engineering, technology and related disciplines.
Exergetic efficiency analysis of hydrogen–air detonation in pulse detonation ...BBIT Kolkata
Exergy losses during the combustion process, heat transfer, and fuel utilization play a vital role in the analysis of the
exergetic efficiency of combustion process. Detonation is thermodynamically more efficient than deflagration mode of
combustion. Detonation combustion technology inside the pulse detonation engine using hydrogen as a fuel is energetic
propulsion system for next generation. In this study, the main objective of this work is to quantify the exergetic efficiency
of hydrogen–air combustion for deflagration and detonation combustion process. Further detonation parameters are
calculated using 0.25, 0.35, and 0.55 of H2 mass concentrations in the combustion process. The simulations have been
performed for converging the solution using commercial computational fluid dynamics package Ansys Fluent solver. The
details of combustion physics in chemical reacting flows of hydrogen–air mixture in two control volumes were simulated
using species transport model with eddy dissipation turbulence chemistry interaction. From these simulations it was
observed that exergy loss in the deflagration combustion process is higher in comparison to the detonation combustion
process. The major observation was that pilot fuel economy for the two combustion processes and augmentation of
exergetic efficiencies are better in the detonation combustion process. The maximum exergetic efficiency of 55.12%,
53.19%, and 23.43% from deflagration combustion process and from detonation combustion process, 67.55%, 57.49%,
and 24.89%, are obtained from aforesaid H2 mass fraction. It was also found that for lesser fuel mass fraction higher
exergetic efficiency was observed.
MODELLING FOR CROSS IGNITION TIME OF A TURBULENT COLD MIXTURE IN A MULTI BURN...ijcsa
This document presents a computational model for determining the cross-ignition time of a turbulent cold mixture in a multi-burner combustor. The model accounts for various parameters that influence heat transfer during the cross-ignition process. Experimental validation was conducted using a simple test rig with two burners. Preliminary results from the experiments show relationships between cross-ignition time and factors like the flow area between burners, distance between burners, and flame properties. Computational fluid dynamics simulations will also be used to further investigate heat transfer in high-velocity regions and validate the model under more conditions.
The understanding of gas geochemical model to reduce the exploration uncertaintyRizal Abiyudo
The various fumaroles areas in the prospect are can be modelled by boiling depletion model and the relation between each of fumaroles. Geothermal waters would boil to create a first set of fumaroles and then the boiled, gas-depleted water outflows to the site of a second set of fumaroles where it boils again, creating fumaroles with gas-depleted chemistry.
EXPERIMENTAL INVESTIGATION ON THERMAL PERFORMANCE OF POROUS RADIANT BURNER AN...BIBHUTI BHUSAN SAMANTARAY
This paper presents the heat transfer characteristics of a
self-aspirating porous radiant burner (SAPRB) that operates
on the basis of an effective energy conversion method between
flowing gas enthalpy and thermal radiation. The temperature
field at various flame zones was measured experimentally by
the help of both FLUKE IR camera and K-type thermocouples.
The experimental setup consisted of a two layered domestic
cooking burner, a flexible test stand attached with six K-type
thermocouples at different positions, IR camera, LPG setup
and a hot wire anemometer. The two layered SAPRB consisted
of a combustion zone and a preheating zone. Combustion zone
was formed with high porosity, highly radiating porous
matrix, and the preheating zone consisted of low porosity
matrix. Time dependent temperature history from
thermocouples at various flame zones were acquired by using
a data acquisition system and the temperature profiles were
analyzed in the ZAILA application software environments. In
the other hand the IR graphs were captured by FLUKE IR
camera and the thermographs were analyzed in the
SMARTView software environments. The experimental results
revealed that the homogeneous porous media, in addition to
its convective heat exchange with the gas, might absorb, emit,
and scatter thermal radiation. The rate of heat transfer was
more at the center of the burner where a combined effect of
both convection & radiation might be realized. The maximum
thermal efficiency was found to be 64% which was having a
good agreement with the previous data in the open literature.
Optimizing Bunsen burner Performance Using CFD AnalysisIJMER
International Journal of Modern Engineering Research (IJMER) is Peer reviewed, online Journal. It serves as an international archival forum of scholarly research related to engineering and science education.
Effect of Ambient Temperature and Composition on Liquid Droplet CombustionIJERA Editor
An unsteady, spherically symmetric, single component, diffusion controlled gas phase droplet combustion
model was developed assuming infinite kinetics and no radiation effects. Finite difference technique was used to
solve time dependent equations of energy and species. Adiabatic flame temperature which is important for
calculating thermodynamic properties was calculated by employing a detailed method. Effects of ambient
temperature and composition on important combustion parameters like adiabatic flame temperature, droplet
mass burning rate, burning constant and droplet lifetime were obtained. Results indicated that flame
temperature, burning constant and mass burning rate increased with an increase in ambient temperature while
the droplet life time decreased. The present gas phase code was used in conjunction with the Olikara and
Borman code for obtaining concentration of important species. Emission results showed that for a 100m nheptane
droplet burning in standard atmosphere, an increase in ambient temperature led to an increase in NO
and CO concentrations and a decrease in CO2 and H2O concentrations. Extinction diameter for a 3000m nheptane
droplet burning in oxygen-helium environment was determined. Also, effects of ambient temperature
and composition were obtained on droplet lifetime and mass burning rate as a function of initial droplet
diameter. The present gas phase model is simple but realistic and can be incorporated in spray combustion
codes.
This document presents a theoretical analysis of the performance of a vapor compression refrigeration system using different refrigerants: R-12, R134a, and R1234yf. The analysis uses a computational model based on the first law of thermodynamics to investigate the effects of evaporating temperature, subcooling, condenser temperature, and liquid-vapor heat exchanger effectiveness on the system's coefficient of performance and refrigerating capacity. The results show that R1234yf has the highest relative capacity increase with increased subcooling and the highest percentage increase in COP. R134a requires the most compressor work. R1234yf is identified as a promising alternative to R134a due to its low global warming potential
Design Criteria for Optimization of the Cross Ignition Process in Gasturbine-...ijscmcj
Reducing of pollutants with simultaneous increase of the gas turbine power, is always a fundamental aim of the Turbine technology. New developed structures and operating systems in the turbine production have been established. In the meanwhile, burning instabilities are still appearing in these systems during a Cross-ignition process (CI), creating pollutants due to high flame temperatures, and are not yet completely investigated.The phenomena of a CI is taking place during operation of malty-burner combustion chambers, when one burner is extinguished and a particular volume of combustible mixture is formed in the distance between this burner and the adjacent lightened one, which considered to be as an ignition path. Cross ignition process should be performed along the ignition path in a particularly controlled small time.So that, no excessive quantities of combustible mixtures will be injected during this time in the combustion chamber. Otherwise, burning instabilities and mechanical wear will be occurred. Depending on this illustration, the Cross Ignition Time (CIT) of an extinguished burner, that will be considered as the evaluation measure for the entire cross-ignition process, should be Possibly as low as its normal ignition time.The main objective of this project is to reproduce constructive criteria for controlling of cross ignition process by influencing the mixing process and heat flux in a defined mixing zone existing along the ignition path.
DESIGN CRITERIA FOR OPTIMIZATION OF THE CROSS IGNITION PROCESS IN GASTURBINE-...ijscmcjournal
Reducing of pollutants with simultaneous increase of the gas turbine power, is always a fundamental aim
of the Turbine technology. New developed structures and operating systems in the turbine production have
been established. In the meanwhile, burning instabilities are still appearing in these systems during a
Cross-ignition process (CI), creating pollutants due to high flame temperatures, and are not yet completely
investigated.
The phenomena of a CI is taking place during operation of malty-burner combustion chambers, when one
burner is extinguished and a particular volume of combustible mixture is formed in the distance between
this burner and the adjacent lightened one, which considered to be as an ignition path.
Cross ignition process should be performed along the ignition path in a particularly controlled small time.
So that, no excessive quantities of combustible mixtures will be injected during this time in the combustion
chamber. Otherwise, burning instabilities and mechanical wear will be occurred.
Depending on this illustration, the Cross Ignition Time (CIT) of an extinguished burner, that will be
considered as the evaluation measure for the entire cross-ignition process, should be Possibly as low as its
normal ignition time.
The main objective of this project is to reproduce constructive criteria for controlling of cross ignition
process by influencing the mixing process and heat flux in a defined mixing zone existing along the ignition
path.
This document presents a theoretical and experimental analysis of a direct-fired double effect lithium bromide/water absorption chiller located at a lighting technology company in Egypt. The chiller has a cooling capacity of 500 tons and uses a parallel flow configuration. Temperature measurements were taken at various points in the chiller components in July 2013 and July 2014. Mathematical equations were developed to model the chiller and estimate the coefficient of performance and heat transfer rates based on temperature and flow rate data. Theoretical and experimental analyses were conducted to evaluate how the COP is affected by factors like heat exchanger effectiveness and circulation ratio. The results show that the chiller's COP was lower in 2014 compared to 2013, possibly due to degradation of the heat ex
Energy performance assessment of boilersUtsav Jain
The document discusses performance testing of boilers. It describes various factors that affect boiler performance over time such as poor combustion, heat transfer fouling, and deteriorated fuel and water quality. Boiler efficiency testing is important to evaluate how efficiency changes from the design value and identify problems. The direct method and indirect method of testing are described. The indirect method involves calculating different heat losses in the boiler system to determine efficiency. Various measurements, instruments, test conditions and computational procedures for conducting boiler performance tests are outlined.
CHARACTERIZATION AND EMISSION ANALYSIS OF PREMIXED AND PREHEATED POROUS RADIA...BIBHUTI BHUSAN SAMANTARAY
This document summarizes an experimental study on the characterization and emission analysis of premixed and preheated porous radiant burners during LPG combustion. Experiments were conducted on 13 different burners made of brass and cast iron with varying geometric parameters like diameter, thickness, pore size, number of pores, and pore distribution. The maximum thermal efficiency obtained was 64.59% for a cast iron burner with the largest diameter and pore distribution. Material, pore geometry, and firing rate significantly affected thermal efficiency and emissions. Burner material, precise pore design, and optimal firing rate are important to improve efficiency while meeting emission standards.
The document discusses energy performance assessment of boilers. It defines key terms like boiler efficiency and evaporation ratio. It describes standards for boiler testing from British, ASME, and Indian standards. It then explains the direct and indirect methods for testing boiler efficiency, including measuring inputs of fuel, air, and outputs of steam. Instruments used for assessment are also outlined. Formats for collecting boiler specifications and performance data are provided. The document calculates boiler efficiency using an example and discusses factors affecting boiler performance.
Analysis of Natural Gas Composition and BTU Content from Fracking OperationsJennifer Maclachlan
This document discusses analyzing the composition and BTU content of natural gas from fracking operations using gas chromatography. It describes how both flame ionization detectors (FID) and thermal conductivity detectors (TCD) are needed to measure the concentrations of hydrocarbon components and inert gases to determine the total BTU value. The analysis can be performed using a gas chromatograph equipped with dual FID/TCD detectors, packed and capillary columns, and temperature programming to separate methane, ethane, and heavier hydrocarbons up to C6 in about 12 minutes to allow calculation of the natural gas heating content.
International Journal of Engineering Research and Applications (IJERA) is an open access online peer reviewed international journal that publishes research and review articles in the fields of Computer Science, Neural Networks, Electrical Engineering, Software Engineering, Information Technology, Mechanical Engineering, Chemical Engineering, Plastic Engineering, Food Technology, Textile Engineering, Nano Technology & science, Power Electronics, Electronics & Communication Engineering, Computational mathematics, Image processing, Civil Engineering, Structural Engineering, Environmental Engineering, VLSI Testing & Low Power VLSI Design etc.
Analysis of the Thermal Efficiency of Condensing Wall-Hung BoilerIJRES Journal
To analyze the impact of the outdoor temperature and humidity on thermal efficiency of the
condensing boiler, the experimental platform is set up based on the condensing boiler and low-temperature
radiantfloor heating system. Using the method of experiment, it’s measured that amount of natural gas, the
temperature of supply and return water, the outdoor temperature and humidity etc. The thermal efficiency is
calculated in different outdoor temperature and humidity. Also it is analyzed that the impact of that the change
of the outdoor temperature and humidity on thermal efficiency. The results show that, when the outdoor
temperature is 8~15℃ and humidity is 30%~70%RH, the impact of the outdoor humidity on thermal efficiency
is very poor. But the impact of outdoor temperature on thermal efficiency is more remarkable. Thermal
efficiency is the higher when the outdoor temperature is the higher.
This document presents a mathematical model for predicting heat losses from a tar sand formation to adjacent formations during thermal recovery processes like steamflooding. The model is developed using conservation of energy principles and heat transfer equations. Sensitivity analyses are performed using the model to analyze how variations in properties of the tar sand formation and steam affect the rate of heat loss. The analyses reveal that increases or decreases in properties like steam and tar sand density can increase or decrease the rate of heat loss. However, some property variations have minimal effect on heat losses. The model can help optimize steam injection parameters to minimize heat losses and improve thermal recovery efficiency.
How to get the combustible stability of the flame.
As well as reducing polluting emissions to the environment.
Work on designing modern combustion burner techniques to avoid combustion problems.
As run boiler performance assessment for energy efficiencyD.Pawan Kumar
The document discusses methods for assessing the energy efficiency of boiler performance. It describes standards from British and ASME for testing boilers under steady load conditions. The direct and indirect methods for determining boiler efficiency are outlined. Instruments required are listed, including flue gas analyzers, temperature indicators, and facilities for analyzing fuel and water samples. Key aspects of indirect method heat balance calculations for a coal-fired boiler are mentioned. Best practices are listed for improving boiler selection, operation and maintenance for energy efficiency.
The document discusses sample conditioning of natural gas for on-stream BTU analysis using gas chromatography. It explains that the natural gas sample must be extracted, transported, and conditioned to be compatible with the analyzer by controlling pressure, flow, removing particulates and liquids. During conditioning, the sample composition must be preserved. The document then discusses various concepts important for understanding sample conditioning like the Joule-Thomson effect, vapor-liquid equilibrium, forms of liquid in pipelines, and how pressure and temperature changes can alter the gas phase composition when liquids are present.
The International Journal of Engineering & Science is aimed at providing a platform for researchers, engineers, scientists, or educators to publish their original research results, to exchange new ideas, to disseminate information in innovative designs, engineering experiences and technological skills. It is also the Journal's objective to promote engineering and technology education. All papers submitted to the Journal will be blind peer-reviewed. Only original articles will be published.
The papers for publication in The International Journal of Engineering& Science are selected through rigorous peer reviews to ensure originality, timeliness, relevance, and readability.
Combustion reactions involve the release or absorption of energy as heat during chemical reactions where products are formed from reactants. A combustion reaction is a chemical reaction where oxygen reacts with a fuel, such as hydrogen, carbon or hydrocarbons, to generate heat and reaction products such as carbon dioxide and water. Stoichiometric coefficients in chemical equations represent equal amounts of each chemical element on both sides of the equation. The air-fuel ratio refers to the ratio of air to fuel, either by mass or moles, involved in a combustion reaction. The theoretical air is the minimum amount of air needed for complete combustion of fuel.
Experimental Evaluation of Refrigerant Mixtures as Substitutes for HFC134aIOSRJMCE
The document describes an experimental evaluation of refrigerant mixtures as substitutes for HFC134a in a 200 liter domestic refrigeration system. The study tested mixtures of propane (R290) and butane (R600a) at different mass ratios, including R600a/R290 at ratios of 70/30, 60/40, and 50/50 by weight percent. The results showed that the R600a/R290 mixture at a ratio of 60/40 performed better than the other mixtures and HFC134a in terms of refrigerating effect and coefficient of performance. Specifically, the 60/40 mixture achieved a refrigerating effect 10% higher than HFC134a at -5°C and 35.
IJREI_Thermodynamic study of R134a in Vapour Compression Refrigeration System...Husain Mehdi
Thermodynamic analysis of an ideal vapour compression refrigeration system is done using refrigerants R134a.This Energy-Exergy analysis is carried out by developed mathematical model. Various parameters are numerically computed are first law efficiency in terms of coefficient of performance (COP) of the system both ideal case and actual experimental and exergetic efficiency and exergy destruction ratio have been computed . The eco-friendly R134a refrigerant gives lower COP than R22. Comparing with R22, R134a takes more compressor power and second law efficiency (exergetic efficiency) of VCRS is also lower than using R22. Due to higher GWP and ODP of R22, R134a can be used for domestic / commercial and industrial applications.
International Journal of Computational Engineering Research(IJCER)ijceronline
International Journal of Computational Engineering Research(IJCER) is an intentional online Journal in English monthly publishing journal. This Journal publish original research work that contributes significantly to further the scientific knowledge in engineering and Technology.
This document discusses boiler efficiency and the factors that affect it. It provides two methods for calculating efficiency - the indirect or loss method, and the direct method. The indirect method calculates efficiency by determining the percentage losses due to factors like flue gas, hydrogen in fuel, moisture, etc. The direct method calculates efficiency as the ratio of useful steam output to heat input. The document also lists ways to improve boiler efficiency, such as oxygen trim systems, flue gas temperature control, and proper water treatment and blowdown control.
Flue gas analisys in industry-Practical guide for Emission and Process Measur...Testo Azerbaijan
Flue gas analisys in industry-Practical guide for Emission and Process Measurements
-Power generation
-Waste disposal
-Stone and clay industry
-Metal industry
-Chemical/petrochemical industry
This document compares the results of a 1-D kinetic model developed in MATLAB and a 0-D thermodynamic model developed in Aspen Plus for predicting syngas composition from biomass steam gasification. The kinetic model combines reaction kinetics and hydrodynamics, while the thermodynamic model uses Gibbs free energy minimization and a quasi-equilibrium approach calibrated with experimental data. A comparison of the model results to experimental data at two steam/biomass ratios showed that the models provide similarly results for main syngas components, though the thermodynamic model shows greater increases in H2 and CO2 and lower decreases in CH4 and CO at higher ratios compared to experiments. The thermodynamic model can be used to analyze overall plant performance but
This document analyzes the performance of a transcritical refrigeration cycle (TRC) enhanced with a dedicated mechanical subcooling system. Three refrigerants are considered: CO2, N2O, and ethane. Results show that while N2O has the highest COP and exergy performance, CO2 has the best economic performance. Adding a subcooler improves the system COP by 30.74% for CO2, 26.48% for N2O, and 36.1% for ethane, while increasing the unit product cost by 9.04%, 8.37%, and 10.63%, respectively. The subcooling is deemed an effective and economical way to improve refrigeration system performance.
Design Criteria for Optimization of the Cross Ignition Process in Gasturbine-...ijscmcj
Reducing of pollutants with simultaneous increase of the gas turbine power, is always a fundamental aim of the Turbine technology. New developed structures and operating systems in the turbine production have been established. In the meanwhile, burning instabilities are still appearing in these systems during a Cross-ignition process (CI), creating pollutants due to high flame temperatures, and are not yet completely investigated.The phenomena of a CI is taking place during operation of malty-burner combustion chambers, when one burner is extinguished and a particular volume of combustible mixture is formed in the distance between this burner and the adjacent lightened one, which considered to be as an ignition path. Cross ignition process should be performed along the ignition path in a particularly controlled small time.So that, no excessive quantities of combustible mixtures will be injected during this time in the combustion chamber. Otherwise, burning instabilities and mechanical wear will be occurred. Depending on this illustration, the Cross Ignition Time (CIT) of an extinguished burner, that will be considered as the evaluation measure for the entire cross-ignition process, should be Possibly as low as its normal ignition time.The main objective of this project is to reproduce constructive criteria for controlling of cross ignition process by influencing the mixing process and heat flux in a defined mixing zone existing along the ignition path.
DESIGN CRITERIA FOR OPTIMIZATION OF THE CROSS IGNITION PROCESS IN GASTURBINE-...ijscmcjournal
Reducing of pollutants with simultaneous increase of the gas turbine power, is always a fundamental aim
of the Turbine technology. New developed structures and operating systems in the turbine production have
been established. In the meanwhile, burning instabilities are still appearing in these systems during a
Cross-ignition process (CI), creating pollutants due to high flame temperatures, and are not yet completely
investigated.
The phenomena of a CI is taking place during operation of malty-burner combustion chambers, when one
burner is extinguished and a particular volume of combustible mixture is formed in the distance between
this burner and the adjacent lightened one, which considered to be as an ignition path.
Cross ignition process should be performed along the ignition path in a particularly controlled small time.
So that, no excessive quantities of combustible mixtures will be injected during this time in the combustion
chamber. Otherwise, burning instabilities and mechanical wear will be occurred.
Depending on this illustration, the Cross Ignition Time (CIT) of an extinguished burner, that will be
considered as the evaluation measure for the entire cross-ignition process, should be Possibly as low as its
normal ignition time.
The main objective of this project is to reproduce constructive criteria for controlling of cross ignition
process by influencing the mixing process and heat flux in a defined mixing zone existing along the ignition
path.
This document presents a theoretical and experimental analysis of a direct-fired double effect lithium bromide/water absorption chiller located at a lighting technology company in Egypt. The chiller has a cooling capacity of 500 tons and uses a parallel flow configuration. Temperature measurements were taken at various points in the chiller components in July 2013 and July 2014. Mathematical equations were developed to model the chiller and estimate the coefficient of performance and heat transfer rates based on temperature and flow rate data. Theoretical and experimental analyses were conducted to evaluate how the COP is affected by factors like heat exchanger effectiveness and circulation ratio. The results show that the chiller's COP was lower in 2014 compared to 2013, possibly due to degradation of the heat ex
Energy performance assessment of boilersUtsav Jain
The document discusses performance testing of boilers. It describes various factors that affect boiler performance over time such as poor combustion, heat transfer fouling, and deteriorated fuel and water quality. Boiler efficiency testing is important to evaluate how efficiency changes from the design value and identify problems. The direct method and indirect method of testing are described. The indirect method involves calculating different heat losses in the boiler system to determine efficiency. Various measurements, instruments, test conditions and computational procedures for conducting boiler performance tests are outlined.
CHARACTERIZATION AND EMISSION ANALYSIS OF PREMIXED AND PREHEATED POROUS RADIA...BIBHUTI BHUSAN SAMANTARAY
This document summarizes an experimental study on the characterization and emission analysis of premixed and preheated porous radiant burners during LPG combustion. Experiments were conducted on 13 different burners made of brass and cast iron with varying geometric parameters like diameter, thickness, pore size, number of pores, and pore distribution. The maximum thermal efficiency obtained was 64.59% for a cast iron burner with the largest diameter and pore distribution. Material, pore geometry, and firing rate significantly affected thermal efficiency and emissions. Burner material, precise pore design, and optimal firing rate are important to improve efficiency while meeting emission standards.
The document discusses energy performance assessment of boilers. It defines key terms like boiler efficiency and evaporation ratio. It describes standards for boiler testing from British, ASME, and Indian standards. It then explains the direct and indirect methods for testing boiler efficiency, including measuring inputs of fuel, air, and outputs of steam. Instruments used for assessment are also outlined. Formats for collecting boiler specifications and performance data are provided. The document calculates boiler efficiency using an example and discusses factors affecting boiler performance.
Analysis of Natural Gas Composition and BTU Content from Fracking OperationsJennifer Maclachlan
This document discusses analyzing the composition and BTU content of natural gas from fracking operations using gas chromatography. It describes how both flame ionization detectors (FID) and thermal conductivity detectors (TCD) are needed to measure the concentrations of hydrocarbon components and inert gases to determine the total BTU value. The analysis can be performed using a gas chromatograph equipped with dual FID/TCD detectors, packed and capillary columns, and temperature programming to separate methane, ethane, and heavier hydrocarbons up to C6 in about 12 minutes to allow calculation of the natural gas heating content.
International Journal of Engineering Research and Applications (IJERA) is an open access online peer reviewed international journal that publishes research and review articles in the fields of Computer Science, Neural Networks, Electrical Engineering, Software Engineering, Information Technology, Mechanical Engineering, Chemical Engineering, Plastic Engineering, Food Technology, Textile Engineering, Nano Technology & science, Power Electronics, Electronics & Communication Engineering, Computational mathematics, Image processing, Civil Engineering, Structural Engineering, Environmental Engineering, VLSI Testing & Low Power VLSI Design etc.
Analysis of the Thermal Efficiency of Condensing Wall-Hung BoilerIJRES Journal
To analyze the impact of the outdoor temperature and humidity on thermal efficiency of the
condensing boiler, the experimental platform is set up based on the condensing boiler and low-temperature
radiantfloor heating system. Using the method of experiment, it’s measured that amount of natural gas, the
temperature of supply and return water, the outdoor temperature and humidity etc. The thermal efficiency is
calculated in different outdoor temperature and humidity. Also it is analyzed that the impact of that the change
of the outdoor temperature and humidity on thermal efficiency. The results show that, when the outdoor
temperature is 8~15℃ and humidity is 30%~70%RH, the impact of the outdoor humidity on thermal efficiency
is very poor. But the impact of outdoor temperature on thermal efficiency is more remarkable. Thermal
efficiency is the higher when the outdoor temperature is the higher.
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Similar to An experimental and kinetic study of syngas-air combustion at elevated temperatures and the effect of water addition (20)
An experimental and kinetic study of syngas-air combustion at elevated temperatures and the effect of water addition
1. An experimental and kinetic study of syngas/air combustion at elevated
temperatures and the effect of water addition
Deepti Singh, Takayuki Nishiie, Saad Tanvir, Li Qiao ⇑
School of Aeronautics & Astronautics, Purdue University, West Lafayette, IN 47907, United States
a r t i c l e i n f o
Article history:
Received 16 May 2011
Received in revised form 22 November 2011
Accepted 30 November 2011
Available online 20 December 2011
Keywords:
Syngas combustion
Elevated temperatures
Water addition
Laminar flame speed
a b s t r a c t
Laminar flame speeds of premixed syngas/air mixtures were measured at various fuel equivalence ratios
(0.6–3.0), H2 content of the fuel, and preheat temperatures (298–500 K) using a spherically expanding
flame configuration. The measured laminar flame speeds were compared with simulations using with
three existing chemical kinetic models – GRI Mech 3.0, H2/CO Davis Mechanism and San Diego mecha-
nism. Reasonable agreement between computations and measurements was achieved at room tempera-
ture that validated the new experimental configuration. However, at higher preheat temperatures
discrepancies between computed and measured values were large, especially for fuel rich mixtures. Addi-
tion of H2O to two fuels (H2/CO = 5/95 and 50/50) up to 40% in the fuel–air mixture was studied to under-
stand the effect of moisture in coal derived syngas. For the H2/CO = 5/95 fuel, flame speed was observed
to increase with up to 20% H2O addition and then to decrease with any further water addition. However,
the higher H2 content fuel (H2/CO = 50/50) only showed a decrease in flame speed with an increasing
water concentration in the fuel–air mixture. The different trends have been explained as a result of
the competing chemical and physical (dilution and thermal) effects of H2O addition on the syngas flames
using sensitivity analyses and by analyzing reaction rates and radical concentrations.
Ó 2011 Elsevier Ltd. All rights reserved.
1. Introduction
Synthetic gas (syngas) is a mixture of carbon monoxide and
hydrogen in various compositions and can be derived from a num-
ber of sources such as coal, biomass gasification or from natural gas
during steam reforming [1]. Syngas is a potential clean fuel and is
already being used in high efficiency gas turbines in the Integrated
Gasification Combined Cycle (IGCC) for power generation. The
composition of syngas is dependent mainly on the fuel source from
which it is derived and it can contain minor constituents such as
CO2, H2O, NH3 and H2S. Variation in its composition can affect
the performance of the system. Therefore, it was considered essen-
tial to study the burning properties of syngas over a wide range of
compositions and with the presence of minor constituents. The
accuracy of kinetic models is critical for the design of clean and
efficient gas turbine combustors. Thus, comprehensive assessment
of the validity of existing chemical kinetic mechanisms under con-
ditions representative of the operating conditions of advanced gas
turbines is required.
Numerous experimental and modeling studies have been re-
ported for syngas. Experimental studies include determination of
species profiles [2,3], ignition delay times [4–7] and laminar flame
speed measurements [8–17]. Several mechanisms have been
developed that can be used to represent the chemical kinetics of
CO–H2 and air mixtures, among which are the GRI Mech 3.0 by
Smith et al. [18], the H2/CO Mech by Davis et al. [19], the San Diego
mechanism by Petrova and Williams [20], a reduced reaction
mechanism for methane and syngas combustion in gas turbines
by Slavinskaya et al. [21], and another H2/CO kinetic mechanism
by Frassoldati et al. [22]. Recently two other mechanisms have
been developed by Li et al. [23] and Sun et al. [8] with the latest
reaction rate constants.
Laminar burning speed is an important parameter that is com-
monly used for validation of chemical kinetics. Laminar burning
speeds of syngas have already been investigated extensively at
normal temperature and pressure, using spherical bombs
[8,10,11,13,17], counter-flow twin flame configurations [12,24]
and Bunsen burners [15,25]. Considerable accuracy in the predic-
tion of the laminar burning speeds has been achieved for normal
temperature and pressure conditions. However, anomalies have
been reported at higher temperatures and pressures that are closer
to the conditions that exist in gas turbines or burners. Natarajan
et al.’s [15] studies of CO–H2 combustion for fuel lean conditions
showed that at high temperatures the measured laminar flame
speeds have large discrepancies with numerical simulations using
GRI Mech 3.0 and H2/CO Davis Mechanism. Furthermore, few stud-
ies (except [26–28]) have considered the effects of minor species
0016-2361/$ - see front matter Ó 2011 Elsevier Ltd. All rights reserved.
doi:10.1016/j.fuel.2011.11.058
⇑ Corresponding author. Tel.: +1 765 494 2040; fax: +1 765 494 0307.
E-mail address: lqiao@purdue.edu (L. Qiao).
Fuel 94 (2012) 448–456
Contents lists available at SciVerse ScienceDirect
Fuel
journal homepage: www.elsevier.com/locate/fuel
2. such as H2O, which could alter the ignition and combustion behav-
ior of syngas.
The motivation of the present paper is to extend flame speed
measurements of syngas for various H2–CO compositions (5%
H2–95% H2), equivalence ratios (0.6–3.0), and high temperatures
(298–500 K) using a spherical flame configuration. In addition,
the effect of addition of H2O to the fuel mixture at high tempera-
ture was investigated. Difference in trends of laminar flame speeds
with increasing water percentage, for fuels containing H2/CO in dif-
ferent ratios has been discussed.
2. Experimental method
The major components of the facility used for the experiments
include a spherical combustion chamber placed inside a high tem-
perature oven, a high voltage spark generator, and a Schlieren opti-
cal system for recording the flame propagation inside the chamber.
A schematic of the experimental facility is shown in Fig. 1. The
spherical combustion chamber is made of stainless steel with an
inside diameter of 36 cm. The chamber is fitted with two diamet-
rically opposed electrodes made of tungsten wire to provide a
spark at the center of the chamber. The gap between these two
electrodes is adjustable and the voltage between the two elec-
trodes is controlled by the high voltage spark generator to provide
the minimum ignition energy. Two quartz windows, with high
durability against pressure and temperature shocks, are mounted
on diametrically opposite ends to provide access for viewing the
flame. The combustion chamber is placed in a customized oven
that can be preheated to a maximum temperature of 650 K using
a precise temperature controller. A Z-type Schlieren imaging sys-
tem has been set up to visualize flame propagation using a high-
speed digital camera with a maximum capture rate up to 6600
frames per second.
At the start of an experiment, the chamber was first vacuumed
and then the reactant mixture was prepared by filling the chamber
with gases at the appropriate partial pressures depending on the
desired mixture composition and test pressure. The prepared mix-
ture was allowed to lay undisturbed for 30 min to allow for any
disturbances to settle and to ensure complete mixing of the fuel
and air by diffusion. A triggering circuit was used to simulta-
neously trigger the recording on the camera and the spark igniter.
For the experiments with water vapor addition, water was
preheated in a chamber to vapor phase before being added to the
fuel mixture in the combustion chamber. Several thermocouples
were installed inside the heated water chamber and on the pipe-
lines between the water chamber and the combustion chamber
to ensure the temperature were above the boiling point of water.
Commercial grade compressed air was used for the experiment
with 99.5% purity. H2 and carbon monoxide were graded at 99.8%
and 99.5% purity respectively. A recent study by Chaos and Dryer
[31] has attributed the deviations between experimental results
from different groups to the presence of iron pentacarbonyl
(Fe(CO)5) impurities in carbon monoxide. Therefore, carbon mon-
oxide stored in aluminum containers was used in the experiments
to ensure the absence of iron pentacarbonyl, a flame inhibitor, as
shown by Rumminger and Linteris [30], that develops over time
in carbon monoxide stored in steel containers.
3. Data processing
Similar to previous measurements of flame speeds [32,33] for
gaseous fuels using a spherical combustion chamber of the same
size, flame radius measurements have been limited to a range of
8 mm < r < 30 mm. The lower limit was chosen to avoid distur-
bances caused by the transient ignition process and the upper limit
was to ensure that the pressure increase inside the chamber was
negligible. The lower limit was determined experimentally in a
manner similar to that employed in the studies of liquid fuels,
which was described in a previous paper [34]. The upper limit of
30 mm was imposed on the radius of flame measurements in
accordance with past flame speed measurement in a similar con-
figuration [32,35–38]. This value corresponds to 16.67% of the
maximum radius and just 0.46% of the total volume of the cham-
ber, which ensures that the pressure rise over this radius is less
than 0.7%. Additionally, Burke et al. [39] has shown that for flame
radius less than 40% of the maximum, the flame speed is affected
by less than 1% due to pressure increase in the chamber. Chen
et al.’s [40] theoretical study of a spherically propagating meth-
ane/air flame also showed that for a ratio of flame radius to maxi-
mum radius lesser than 0.2, the effect of compression induced flow
is almost negligible.
Under these assumptions, the local stretched flame speed and
flame stretch is given by the following quasi-steady expressions
proposed by Strehlow and Savage [41],
Pressure
Gauge
Gas
Cylinders
Ignition System
Oven
Mercury
Lamp
Concave
Mirror
Electrodes
Fuel Chamber
Heated
Line
Lens
High-speed
Digital Camera
Pressure Transducer &
Oscilloscope
Quartz
Window
Vacuum
Pump
Fig. 1. A schematic of the experimental facility.
D. Singh et al. / Fuel 94 (2012) 448–456 449
3. SL ¼
qb
qu
drf
dt
ð1Þ
K ¼
2
rf
drf
dt
ð2Þ
where SL is the unburned gas speed and K is the flame stretch. The
ratio of the burned gas to the unburned gas density was computed
using the NASA Chemical Equilibrium Applications code under the
assumption of adiabatic constant pressure combustion [42].
For small stretch rates, the stretched flame speed data can be
extrapolated linearly to zero stretch to obtain the unstretched lam-
inar flame speed, SL1. The following equation proposed by Mark-
stein [43] and Clavin [44] provides this linear relationship:
SL ¼ SL1 À LuK ð3Þ
where Lu is the Markstein length.
This widely-used linear relation (Eq. (3)) is however subject to
the limitations of small stretch rate [45]. For moderate stretch
rates, the following non-linear relation based on a model devel-
oped by Ronney and Sivashinsky [46] for quasi-steady, outwardly
propagating spherical flames is more appropriate to obtain the un-
stretched laminar flame speed (Sb1):
Sb
Sb1
2
ln
Sb
Sb1
2
¼ À
2LbK
Sb1
ð4Þ
where Sb is the stretched flame speed of the burned gases and Lb is
the burned gas Markstein length. The unstretched flame speed rel-
ative to unburned gases (SL1) is related to Sb1 by the ratio of the
burned and unburned gas density. For most conditions, the flame
speeds obtained by linear and non-linear extrapolation were very
similar. The values of flame speeds presented below are obtained
using non-linear extrapolation.
4. Computational method
Numerical simulations of steady, laminar, freely propagating 1-
D premixed flames were carried out using the PREMIX [47] module
of the CHEMKIN 4.1 [48] software. Multi-component diffusion
coefficients were used to evaluate the transport properties of the
gas mixture. Computational grid and grid tolerance parameters
were reduced to 0.1 or lower to ensure accuracy.
Three reaction mechanisms – GRI Mech 3.0 [49], H2/CO kinetic
model proposed by Davis and Law [50] and San Diego mechanism
[20] have been used to numerically simulate the laminar burning
speeds. The GRI Mech 3.0 contains 53 species and 325 reactions
and has been validated by various experimental studies for the
accurate prediction of laminar burning speeds, species profiles
and ignition delay times of methane–air mixtures and CO–H2/air
mixtures [18]. The second mechanism which is specific to H2/CO
combustion consists of 14 species and 30 reactions [19]. It has been
extensively validated for a large number of combustion parameters
and is widely cited in literature. It is now the basis of the USC Mech
II [51] reaction model for C1–C4 kinetics. The San Diego mecha-
nism consists of 38 species and 235 reactions and has been devel-
oped to represent the behavior of various small hydrocarbons
containing up to 3 carbon atoms, in conditions that occur in flames,
high temperature ignition and detonations. This mechanism has
been verified with several gases and fuels to give fairly accurate
predictions [52]. Simulations from this mechanism were verified
against burning speeds and auto-ignition characteristics of pre-
mixed CO/H2 flames and were shown to have excellent agreement
with data available in literature.
5. Results and discussion
The unstretched flame speeds of different H2–CO mixtures are
presented below as a function of equivalence ratio at atmospheric
pressure and normal and elevated temperatures. The measured
speeds were compared with the numerical simulations using GRI
Mech 3.0 [18], H2/CO Mech [19] and San Diego [20] kinetic mech-
anisms, as well as experimental data from literature. Furthermore,
laminar flame speeds of syngas mixtures with addition of water are
reported along with comparisons with computational results and
an analysis of the results. In the following discussion the laminar
flame speed refers to the unstretched speeds.
5.1. Validation: flame speeds at room temperature
Experiments were performed for various compositions of syn-
gas at 298 K. These results were compared with the experimental
data in the literature with the intention of providing a validation
for the current experimental setup. Fig. 2 shows the measured
and predicted flame speeds for syngas/air mixtures a function of
fuel equivalence ratio at 298 K and 1 atm. Also shown are the
experimental data of Sun et al. [8], McLean et al. [11] acquired from
spherically propagating flames and Natarajan et al. [15] using Bun-
sen burner flames, where available. For the high hydrogen content
(HHC) syngas mixtures (75% H2–25% CO), no data have been re-
ported previously.
For the 5% H2–95% CO mixture, all the measurements made
using spherically propagating flames (Sun et al. [8] , McLean
et al. [11] and the present results) are in good agreement with each
other. The values measured by Natarajan et al. [15] are slightly
higher than the present measurement and other measurements
made with spherical flame configurations over equivalence ratios
ranging from 0.6–0.9. Similarly for the 25% H2–75% CO mixture
and the equimolar mixture of H2–CO (50–50%), the present mea-
surement are in good agreement with those measured by Sun
et al. [8], McLean et al. [11] and Natarajan et al. [15]. On compari-
son of the computational results, it can be seen that the H2/CO Da-
vis mechanism and the San Diego mechanism can simulate the
experimentally determined flame speeds with better accuracy as
compared with the GRI Mech-3.0 mechanism. The predictions by
the GRI Mech 3.0 [18] are higher than the predictions by the other
two mechanisms and the difference is most significant for fuel rich
mixtures.
Fig. 2. Laminar flame speeds of various compositions of H2–CO mixtures for
different equivalence ratios at 298 K and 1 atm. Lines represent simulations using
different mechanisms and symbols represent experimental data.
450 D. Singh et al. / Fuel 94 (2012) 448–456
4. With increase in percentage of hydrogen in the fuel mixture,
there is an increase in the flame speeds at all equivalence ratios,
as expected. The equivalence ratio corresponding to the maximum
burning speed shifts towards the fuel lean side with increase in
hydrogen content in the fuel. The flame speed peaks at approxi-
mately / = 3.0 at a value close to 65 cm/s for a 5% H2–95% CO mix-
ture whereas the peak occurs at / = 1.8 for the 75% H2–25% CO fuel.
The shifting of the peak from rich to lean going from 5% H2 to 75%
H2 in the fuel mixture is because addition of H2 to CO results in a
kinetic effect through the reaction CO + OH = CO2 + H. The flame
speed has the highest sensitivity to this reaction (as is discussed
in Section 5.4). However, this kinetic effect is much stronger for
small percentages of H2 and possibly overshadows the decrease
in the flame speed due to reduced adiabatic flame temperatures
for the rich mixtures. With higher percentages of H2, this effect sat-
urates and the peak flame speed is closer to where it occurs for
pure H2 flames.
5.2. Effects of preheat temperature
To examine the effect of preheat temperature on flame speed
and chemical kinetics, experiments were conducted at elevated
temperatures of 400 K and 500 K for the 50% H2–50% CO mixture.
The results are shown in Fig. 3. With increase in preheat tempera-
ture (300–500 K), there is an increase in flame speed as expected.
At a preheat temperature of 500 K, the present measurements at
fuel-lean conditions are lower than the measurements made by
Natarajan et al. [14]. The discrepancy between the measured and
computed flame speeds also becomes significant at 500 K, espe-
cially at fuel rich conditions. All the mechanisms over predict mea-
sured flame speeds.
Discrepancies between measured and predicted flame speeds at
higher preheat temperatures have been reported by others for syn-
gas mixtures. Natarajan et al. [15] show that existing kinetics over-
predict flame speeds at temperatures above 400 K; and the
discrepancy increases with increasing preheat temperature. Note
these experiments were conducted primarily for fuel lean condi-
tions. The discrepancies could be due to the inaccurate representa-
tion of reaction rates of certain reactions at higher temperatures.
Motivated by this, we performed sensitivity analyses of flame
speed with respect to reaction rates for the 50% H2–50% CO mix-
ture at / = 3.0 at 298 K, 400 K and 500 K, respectively. These results
are shown in Fig. 4 and highlight the reactions to which the flame
speed is most sensitive. As the preheat temperature increases, the
sensitivity coefficient for these reactions increase: H2 + O = OH + H,
H2 + OH = H2O + H and H + O2(+M) = HO2 + M. In particular, the last
one is a chain recombination reaction involving third bodies. It
might be useful to further look at the reaction rates of these reac-
tions at higher temperatures.
5.3. Effect of addition of H2O
Coal derived syngas from most gasifiers typically has a moisture
content of 6–20% [29]. This motivated us to study the effect of
water addition on flame speed and chemical kinetics. Stoichiome-
tric fuel mixtures containing H2–CO in the ratios – 5:95 and 50:50
were used to study the physical and chemical effect of H2O in syn-
gas. All the experiments were conducted at 400 K. Water was pre-
heated in a heated fuel line to vapor phase before being added to
the fuel mixture into the combustion chamber.
Fig. 5 shows the measured and predicted flames speeds for var-
ious percentages of water addition to the fuel mixture. An initial
increase in flame speed is observed with up to 20% H2O addition
for the fuel mixture containing H2–CO in a 5:95 ratio. This result
is similar to observations made by Das et al. [53] at 323 K. The
flame speed from the present measurements at the peak was 28%
higher than the flame speed for a dry H2–CO mixture. Beyond that
any addition of water results in a decrease in the flame speed.
However, such a trend is not observed for the equimolar mixture
of H2–CO. The flame speed decreases monotonically with H2O
addition in the fuel mixture. The H2/CO Davis and San Diego mech-
anisms have better predictions over most of the range of fuel-
water mixtures considered for the H2:CO-5:95 and 50:50 ratio.
The behavior for low H2 content fuels with H2O addition was
further analyzed to understand the cause of this initial increase
in flame speed observed. Fig. 6 shows the calculated adiabatic
flame temperature as a function of H2O percentage in the fuel mix-
ture, for both 5:95 and 50:50 H2/CO compositions. For both mix-
tures, the adiabatic flame temperature decreases with increase in
H2O addition, due to the large heat capacity of H2O, reflecting the
physical dilution effect. The decreasing flame temperature should
result in a corresponding decrease in flame speed. Therefore, the
initial increase in flame speed for low H2 content fuels with H2O
addition could be due to the dominance of a chemical effect
Fig. 3. Comparison of laminar flame speeds for 50% H2–50% CO at different preheat
temperatures at 1 atm. Lines represent simulations using different mechanisms and
symbols represent experimental data.
Fig. 4. Normalized sensitivity coefficient of flame speed with respect to the reaction
rate for H2/CO (50:50)/airflames at / = 3.0 with varying preheat temperature. The
sensitivity coefficients were calculated using the San Diego mechanism.
D. Singh et al. / Fuel 94 (2012) 448–456 451
5. (e.g., chemical reaction involving H2O to produce H, O and OH rad-
icals) over this decreasing physical effect [53]. This is discussed in
the following.
5.4. Chemical effect of water addition
To understand the chemical effect of water addition, we first
examined the concentrations of the important radicals including
H, O, and OH in the reaction zone. Previous studies have shown a
strong correlation between flame speed and the maximum concen-
tration of H and OH radicals in the reaction zone of premixed
hydrogen flames [32,54,55]. Figs. 7 and 8 show the profiles of the
intermediate species for H2–CO (5:95)/H2O/air and H2–CO(50–
50)/H2O/air flames respectively, at 1 atm and 400 K using the San
Diego Mechanism. For the former flame, the maximum concentra-
tion of H and OH radicals increase with H2O addition up to 20% in
the fuel mixture, beyond which the H and OH radical concentra-
tions decreases with further H2O addition. This indicates that a
small amount of water addition produces more H and OH radicals
in the reaction zone than the dry fuel. However, the maximum con-
centration of H and OH radicals decrease monotonically for
increasing water percentage to the fuel with 50% H2–50% CO. For
both cases, the maximum concentration of O radical decreases as
the water percentage increases. The findings here, which are con-
sistent with the above mentioned earlier studies [32,54,55], par-
tially explain why a small amount of water addition increases
flame speed. That is, an increase in H or OH concentrations would
result in an increase in flame speed.
To further look at the kinetic effect of water addition, we per-
formed sensitivity analysis of flame speed using the San Diego
mechanism. The normalized sensitivity coefficients with respective
to the reaction rates of the most important reactions are shown in
Fig. 9 for the 5% H2–95% CO/air mixture. The CO + OH = CO2 + H
(R7) reaction has the highest sensitivity and has an increasing ef-
fect on the flame speed with H2O addition up to 30%. It can be seen
that the addition of H2O increases the sensitivity of the chain
branching reactions – H + O2 = OH + O (R1) and H2O + O = 2OH
(R2), both resulting in an increase in OH radical production. There
is decreased sensitivity of the reactions H2 + O = OH + H (R3) and
HO2 + H = 2OH (R4). The sensitivity to the three-body chain termi-
nation reactions H + OH + M = H2O + M (R5), involving the con-
sumption of OH and H radicals, increases with increase in
percentage of H2O. Since reaction R5 has a negative sensitivity,
an increase in its sensitivity indicates a decrease in flame speed
with increased reaction rate.
To understand the difference in behavior of the higher hydrogen
content fuel, a similar analysis was conducted for the 50% H2–50%
CO mixture (Fig. 10). The major difference is the effect of the reac-
tion H2 + OH = H2O + H (R8). In the case of the fuel with H2/CO in
the ratio of 5/95, this reaction has a slight negative sensitivity coef-
ficient on flame speed. With increase in percentage of H2O the
reaction is driven in the reverse direction, generating greater num-
ber of OH radicals. On the other hand, for the 50/50 ratio of H2/CO,
the reaction has a strong positive influence. This is because of high-
er concentration of H2 that could drive the reaction in the forward
direction consuming the OH radicals. The sensitivity of R7 is re-
duced comparatively and is comparable to the sensitivities of R1
and R2. There is a change in sensitivity of the reactions only with
an initial increase in H2O percentage up to 10% after which the sen-
sitivities remain unchanged. Also, the reaction R2 has an extremely
low sensitivity for the 50/50 H2/CO fuel; whereas it was significant
for the previous case indicating that this could be responsible for
the difference in behavior of the 2 fuels.
To further understand the chemical effect of water addition,
reactions rates were studied, particularly those reactions on which
the fuel flow rate has maximum sensitivity. Fig. 11 shows reaction
rates of H2/CO (5/95)/H2O/air mixtures with H2O content varying
from 0–40%. From the reaction rate profiles, it can be seen that
reaction R7 has the highest reaction rate followed by reaction R1.
Flame speed has the highest sensitivity to the reaction rate of R7
and this rate almost doubles with 20% addition of water. With
any further addition of water, the reaction rate starts to show a
very slight decrease. This increase in reaction rate is created by
the increased OH radical pool as is seen from the species profiles
(Fig. 7). OH radical concentrations show an increase for up to
20% H2O in the fuel mixture and then slightly decrease. Increased
H2O concentration up to 20% also has an increasing effect on the
reaction rates of most of the reactions that result in addition of rad-
icals to the OH pool except reaction R8. The reaction R8 has a neg-
ative reaction rate and its rate increases significantly with increase
in the percentage of water. The net concentration of OH is a resul-
tant from these reactions causing an increase with up to 20% water
addition as is seen from Fig. 7.
In summary, from the above analysis of the reaction rates, rad-
ical profiles and sensitivities, it can be seen that addition of water
Fig. 5. Laminar flame speeds for H2/CO(5:95)/H2O/air flames and H2/CO (50:50)/
H2O/air at 1 atm and 400 K. Solid lines, dashed and dashed dotted lines represent
simulations using GRI Mech 3.0, H2/CO Davis and San Diego models respectively,
and symbols represent experimental data.
Fig. 6. Calculated adiabatic flame temperature as a function of H2O percentage in
various compositions of H2/CO/air mixtures.
452 D. Singh et al. / Fuel 94 (2012) 448–456
6. to the fuel mixture (H2/CO = 5/95) increases the concentration of
the OH radicals, which control the main reaction that affects flame
speed. The reaction rates depend on reactant temperatures and
concentrations of the radicals. With H2O addition to the fuels,
the flame temperatures decrease whereas the OH radical concen-
trations increase. Therefore, it can be said that for up to 20% H2O
in the fuel mixture, the chemical effect of the increase in OH radi-
cals is stronger than the thermal and dilution effects of reduction
in temperature. This results in an increase in the flame speed. Be-
yond this, the dilution of the fuel and hence, lowering of the flame
and burned gas temperature dominates and the resultant effect is a
lowering in the flame speed. As opposed to this, the higher H2 con-
tent fuel (H2/CO = 50/50) does not demonstrate the dominance of
chemical effect. The dominant effect on flame speed is the ther-
mal/dilution effect of H2O presence in the fuel resulting in lower-
ing reaction rates, and therefore, flame speed s.
Fig. 7. Profiles of the major radical concentrations for H2/CO (5:95)/H2O/air mixtures at 400 K and 1 atm. (a) 0% H2O; (b) 10% H2O; (c) 20% H2O; (d) 30% H2O; (e) 40% H2O.
D. Singh et al. / Fuel 94 (2012) 448–456 453
7. Fig. 8. Profiles of the major radical concentrations for H2/CO (50:50)/H2O/air mixtures at 400 K and 1 atm. (a) 0% H2O; (b) 10% H2O; (c) 20% H2O.
Fig. 9. Normalized sensitivity coefficient of flame speed with respect to the reaction rate for H2/CO (5:95)/air flames with varying concentration of water (0–40%). The
mechanism used is the San Diego mechanism.
454 D. Singh et al. / Fuel 94 (2012) 448–456
8. Fig. 10. Normalized sensitivity coefficient of flame speed with respect to the reaction rate for H2/CO (50:50)/air flames with varying concentration of water (0–40%). The
mechanism used is the San Diego mechanism.
Fig. 11. Reaction rates of the most important reactions for H2/CO (5:95)/air mixtures with varying percentages of H2O (0–40%). (a) 0% H2O; (b) 20% H2O; (c) 30% H2O; (d) 40%
H2O.
D. Singh et al. / Fuel 94 (2012) 448–456 455
9. 6. Conclusions
Laminar flame speeds of four compositions of syngas, with H2
content varying from 5% to 75%, were measured at room and ele-
vated temperatures using spherically expanding flames. The room
temperature measurements were in good agreement with the
experimental data in the literature, providing a validation of
the present experimental apparatus. Large discrepancies between
the measured and predicted flame speeds, however, were observed
at higher preheat temperatures, especially for fuel rich conditions.
The discrepancies could be caused by the inaccurate representation
of reaction rates of certain reactions at higher temperatures. Never-
theless, more investigation is needed on the effect of preheat tem-
perature on flame speed and chemical kinetics. Regarding water
addition, the low hydrogen content syngas mixture demonstrated
an increasing trend with increasing percentage of H2O in the fuel
mixture, up to 20% H2O addition. Beyond this percentage, the trend
reversed and followed the expected behavior due to reduced flame
temperature. However, for the high hydrogen content syngas mix-
ture, a straight forward inverse correlation between flame speed
and H2O addition to the fuel mixture was observed. These different
trends are attributed to the competition between the chemical effect
and the physical effect (thermal and dilution) of water addition.
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