Some folks argue for Bernard King, but he was smaller and had more confined scoring areas than Anthony.
The term "confined conditions" is the opposite of "free conditions"
Work on a long stream of air under the teeth on the F
conFFFFFFined
(memory trick: the teeth confine the lower lip)
Confined reacting turbulent jets / are widely employed / in industrial furnaces. (4 stresses in the 1st group) / 2 stresses in the 2nd/ 2 stresses in the 3rd
Confined reacting turbulent jets are widely employed in industrial furnaces. /pl/ practice Play, pluck, complain, employ (memory trick: just lip-lip, the teeth can't be employed)
an inquiry into unfamiliar or questionable activities
This paper / presents the results / of an experimental investigation / of mixing characteristics / and the resulting chemical composition / in a confined, / non-reacting turbulent jet.
This paper presents the results of an experimental investigation of mixing characteristics and the resulting chemical composition in a confined, non-reacting turbulent jet.
produced by reactions involving atomic or molecular changes
This paper presents the results of an experimental investigation of mixing characteristics and the resulting chemical composition in a confined, non-reacting turbulent jet.
the way in which someone or something is put together
This paper presents the results of an experimental investigation of mixing characteristics and the resulting chemical composition in a confined, non-reacting turbulent jet.
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
at right angles to the plane of the horizon or a base line
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
the degree of hotness or coldness of a body or environment
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
a projecting spout from which a fluid is discharged
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
an area that is in the middle of some larger region
The apparatus consists of: (i) a 2ft diameter 6ft long cylindrical vertical exhaust duct that carries 328.15K slight hot air at co-flow velocities ranging from 0.11 to 1.11 m/s; (ii) ambient temperature high velocity air jet containing a NO tracer gas is injected by a ¼ inch nozzle in the center of the vertical duct.
an outline of something, especially a face from the side
Temperature, composition and velocity profile measurements are made along the length of the jet to determine the extent of entrainment and the dilution of the jet fluid as a function of the co-flow and jet flow velocities.
assigning numbers to phenomena according to a rule
Temperature, composition and velocity profile measurements are made along the length of the jet to determine the extent of entrainment and the dilution of the jet fluid as a function of the co-flow and jet flow velocities.
the linear extent in space from one end to the other
Temperature, composition and velocity profile measurements are made along the length of the jet to determine the extent of entrainment and the dilution of the jet fluid as a function of the co-flow and jet flow velocities.
find out or learn with certainty, as by making an inquiry
Temperature, composition and velocity profile measurements are made along the length of the jet to determine the extent of entrainment and the dilution of the jet fluid as a function of the co-flow and jet flow velocities.
Temperature, composition and velocity profile measurements are made along the length of the jet to determine the extent of entrainment and the dilution of the jet fluid as a function of the co-flow and jet flow velocities.
Temperature, composition and velocity profile measurements are made along the length of the jet to determine the extent of entrainment and the dilution of the jet fluid as a function of the co-flow and jet flow velocities.
Temperature, composition and velocity profile measurements are made along the length of the jet to determine the extent of entrainment and the dilution of the jet fluid as a function of the co-flow and jet flow velocities.
By comparison of the entrainment rate in free and confined jet, it is found that the confinement effect becomes more prominent as the co-flow velocity is reduced and the jet velocity is increased.
By comparison of the entrainment rate in free and confined jet, it is found that the confinement effect becomes more prominent as the co-flow velocity is reduced and the jet velocity is increased.
a phenomenon that is caused by some previous phenomenon
By comparison of the entrainment rate in free and confined jet, it is found that the confinement effect becomes more prominent as the co-flow velocity is reduced and the jet velocity is increased.
By comparison of the entrainment rate in free and confined jet, it is found that the confinement effect becomes more prominent as the co-flow velocity is reduced and the jet velocity is increased.
a process of becoming larger or longer or more numerous
By comparison of the entrainment rate in free and confined jet, it is found that the confinement effect becomes more prominent as the co-flow velocity is reduced and the jet velocity is increased.
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
of the immediate past or just previous to the present time
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
the quality of having the means or skills to do something
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
a substance that can be consumed to produce energy
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
examine and note the similarities or differences of
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
being approximately average or within certain limits
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
a reaction of a substance with oxygen to give heat and light
Exhaust(or Flue) gas recirculation system has received much attention in recent years due to its ability to reduce both fuel consumption and mainly NOx emissions compared to normal combustion.
Although the recirculation of exhaust gas causes to lower temperature, Internal Exhaust Gas Recirculation (IEGR) has been found to be the most effective technique in controlling NOx emissions [1].
producing or capable of producing an intended result
Although the recirculation of exhaust gas causes to lower temperature, Internal Exhaust Gas Recirculation (IEGR) has been found to be the most effective technique in controlling NOx emissions [1].
a practical method or art applied to some particular task
Although the recirculation of exhaust gas causes to lower temperature, Internal Exhaust Gas Recirculation (IEGR) has been found to be the most effective technique in controlling NOx emissions [1].
Although the recirculation of exhaust gas causes to lower temperature, Internal Exhaust Gas Recirculation (IEGR) has been found to be the most effective technique in controlling NOx emissions [1].
This paper presents the results of an experimental and numerical investigation of mixing characteristics and the resulting chemical composition of a confined, non-reacting turbulent jet inside the EGR through adding NO tracer gas.
As a result, the mixing distribution of the gas before entering the combustor strongly depends on the jet interaction between high velocity air jet and hot air to be simulated as exhaust gas under this configuration.
As a result, the mixing distribution of the gas before entering the combustor strongly depends on the jet interaction between high velocity air jet and hot air to be simulated as exhaust gas under this configuration.
reproduced or made to resemble; imitative in character
As a result, the mixing distribution of the gas before entering the combustor strongly depends on the jet interaction between high velocity air jet and hot air to be simulated as exhaust gas under this configuration.
As a result, the mixing distribution of the gas before entering the combustor strongly depends on the jet interaction between high velocity air jet and hot air to be simulated as exhaust gas under this configuration.
a mode of being or form of existence of a person or thing
The essential conditions for achieving quickly uniform gas redistribution inside FGR are the injection of air jet with high momentum and the high recirculation of hot air.
The essential conditions for achieving quickly uniform gas redistribution inside FGR are the injection of air jet with high momentum and the high recirculation of hot air.
The essential conditions for achieving quickly uniform gas redistribution inside FGR are the injection of air jet with high momentum and the high recirculation of hot air.
It shows that there are significant differences between confined turbulent jet and free turbulent jet flow because of the existence of recirculating flow or back flow entrained by the jet in the previous studies.
It shows that there are significant differences between confined turbulent jet and free turbulent jet flow because of the existence of recirculating flow or back flow entrained by the jet in the previous studies.
It shows that there are significant differences between confined turbulent jet and free turbulent jet flow because of the existence of recirculating flow or back flow entrained by the jet in the previous studies.
keep in safety and protect from harm, loss, or destruction
Also, the mixing and entrainment of the confined jet is different from free jets because the momentum in confined jet is not conserved and the adverse pressure gradient is generated by the confinement.
Also, the mixing and entrainment of the confined jet is different from free jets because the momentum in confined jet is not conserved and the adverse pressure gradient is generated by the confinement.
Also, the mixing and entrainment of the confined jet is different from free jets because the momentum in confined jet is not conserved and the adverse pressure gradient is generated by the confinement.
Also, the mixing and entrainment of the confined jet is different from free jets because the momentum in confined jet is not conserved and the adverse pressure gradient is generated by the confinement.
Also, the mixing and entrainment of the confined jet is different from free jets because the momentum in confined jet is not conserved and the adverse pressure gradient is generated by the confinement.
Although numerous and experimental works on a single turbulent jet are available in the literature, very few investigations have been conducted on the flow structure and passive scalar transport of confined turbulent jet with co-flow.
obtainable or accessible and ready for use or service
Although numerous and experimental works on a single turbulent jet are available in the literature, very few investigations have been conducted on the flow structure and passive scalar transport of confined turbulent jet with co-flow.
writings in a particular style on a particular subject
Although numerous and experimental works on a single turbulent jet are available in the literature, very few investigations have been conducted on the flow structure and passive scalar transport of confined turbulent jet with co-flow.
Although numerous and experimental works on a single turbulent jet are available in the literature, very few investigations have been conducted on the flow structure and passive scalar transport of confined turbulent jet with co-flow.
Although numerous and experimental works on a single turbulent jet are available in the literature, very few investigations have been conducted on the flow structure and passive scalar transport of confined turbulent jet with co-flow.
Although numerous and experimental works on a single turbulent jet are available in the literature, very few investigations have been conducted on the flow structure and passive scalar transport of confined turbulent jet with co-flow.
Although numerous and experimental works on a single turbulent jet are available in the literature, very few investigations have been conducted on the flow structure and passive scalar transport of confined turbulent jet with co-flow.
This is due to the complicated characteristics of the confined turbulent jet with co-flow while considerable experimental and numerical efforts have been investigated on the study of turbulent jets issuing into a free environment.
This is due to the complicated characteristics of the confined turbulent jet with co-flow while considerable experimental and numerical efforts have been investigated on the study of turbulent jets issuing into a free environment.
This is due to the complicated characteristics of the confined turbulent jet with co-flow while considerable experimental and numerical efforts have been investigated on the study of turbulent jets issuing into a free environment.
This is due to the complicated characteristics of the confined turbulent jet with co-flow while considerable experimental and numerical efforts have been investigated on the study of turbulent jets issuing into a free environment.
This is due to the complicated characteristics of the confined turbulent jet with co-flow while considerable experimental and numerical efforts have been investigated on the study of turbulent jets issuing into a free environment.
This is due to the complicated characteristics of the confined turbulent jet with co-flow while considerable experimental and numerical efforts have been investigated on the study of turbulent jets issuing into a free environment.
To make the similarity parameter, it is assumed that the entrainment and mass flow rate between the nozzle and the duct are identical to free jet flow.
To make the similarity parameter, it is assumed that the entrainment and mass flow rate between the nozzle and the duct are identical to free jet flow.
To make the similarity parameter, it is assumed that the entrainment and mass flow rate between the nozzle and the duct are identical to free jet flow.
Curtet and Ricou[5] progressed experimental work of the isothermally axis-symmetric confined jets to verify the theoretical approach of the Craya-Curtet number.
Curtet and Ricou[5] progressed experimental work of the isothermally axis-symmetric confined jets to verify the theoretical approach of the Craya-Curtet number.
concerned with hypotheses and not practical considerations
Curtet and Ricou[5] progressed experimental work of the isothermally axis-symmetric confined jets to verify the theoretical approach of the Craya-Curtet number.
uninterrupted in time and indefinitely long continuing
The experimental studies by Becker et al.[6] have shown that the flow and mixing characteristics of constant-density confined jets(the only functions of the Craya-Curtet number) measure mean velocity and concentration to be used in light scattering methods developed by Rosensweig.
The experimental studies by Becker et al.[6] have shown that the flow and mixing characteristics of constant-density confined jets(the only functions of the Craya-Curtet number) measure mean velocity and concentration to be used in light scattering methods developed by Rosensweig.
The experimental studies by Becker et al.[6] have shown that the flow and mixing characteristics of constant-density confined jets(the only functions of the Craya-Curtet number) measure mean velocity and concentration to be used in light scattering methods developed by Rosensweig.
The experimental studies by Becker et al.[6] have shown that the flow and mixing characteristics of constant-density confined jets(the only functions of the Craya-Curtet number) measure mean velocity and concentration to be used in light scattering methods developed by Rosensweig.
a way of doing something, especially a systematic way
The experimental studies by Becker et al.[6] have shown that the flow and mixing characteristics of constant-density confined jets(the only functions of the Craya-Curtet number) measure mean velocity and concentration to be used in light scattering methods developed by Rosensweig.
progress or evolve through a process of natural growth
The experimental studies by Becker et al.[6] have shown that the flow and mixing characteristics of constant-density confined jets(the only functions of the Craya-Curtet number) measure mean velocity and concentration to be used in light scattering methods developed by Rosensweig.
They introduced the kinematic mean velocity uk and dynamic mean velocity ud for understanding the physical meaning of the Craya-Curtet number as well as the theoretical calculations of concentration in confined turbulent jet fields.
involving the body as distinguished from the mind or spirit
They introduced the kinematic mean velocity uk and dynamic mean velocity ud for understanding the physical meaning of the Craya-Curtet number as well as the theoretical calculations of concentration in confined turbulent jet fields.
the message that is intended or expressed or signified
They introduced the kinematic mean velocity uk and dynamic mean velocity ud for understanding the physical meaning of the Craya-Curtet number as well as the theoretical calculations of concentration in confined turbulent jet fields.
Hill[8][9] estimated the characteristics of mean velocity field in an isothermal homogeneous-confined turbulent jet flow for jet mixing by different cross section areas through considering differential integral methods.
a marking that consists of lines that intersect each other
Hill[8][9] estimated the characteristics of mean velocity field in an isothermal homogeneous-confined turbulent jet flow for jet mixing by different cross section areas through considering differential integral methods.
one of several parts or pieces that fit with others
Hill[8][9] estimated the characteristics of mean velocity field in an isothermal homogeneous-confined turbulent jet flow for jet mixing by different cross section areas through considering differential integral methods.
the extent of a two-dimensional surface within a boundary
Hill[8][9] estimated the characteristics of mean velocity field in an isothermal homogeneous-confined turbulent jet flow for jet mixing by different cross section areas through considering differential integral methods.
Hill[8][9] estimated the characteristics of mean velocity field in an isothermal homogeneous-confined turbulent jet flow for jet mixing by different cross section areas through considering differential integral methods.
a quality that distinguishes between similar things
Hill[8][9] estimated the characteristics of mean velocity field in an isothermal homogeneous-confined turbulent jet flow for jet mixing by different cross section areas through considering differential integral methods.
He suggested that the mean velocity profiles in self-preserving regions of the confined turbulent jets could be estimated from the results of circular free turbulent jet flow.
keep in safety and protect from harm, loss, or destruction
He suggested that the mean velocity profiles in self-preserving regions of the confined turbulent jets could be estimated from the results of circular free turbulent jet flow.
He suggested that the mean velocity profiles in self-preserving regions of the confined turbulent jets could be estimated from the results of circular free turbulent jet flow.
an area or region distinguished from adjacent parts
Barchilon et al.[10] show that the recirculation zone occurs in cylindrical ducts through measuring mean velocities, the variation of wall static pressures, the size of the recirculation zone in water flow as well as the root mean square values of the axial velocity fluctuation in air flow.
Barchilon et al.[10] show that the recirculation zone occurs in cylindrical ducts through measuring mean velocities, the variation of wall static pressures, the size of the recirculation zone in water flow as well as the root mean square values of the axial velocity fluctuation in air flow.
Barchilon et al.[10] show that the recirculation zone occurs in cylindrical ducts through measuring mean velocities, the variation of wall static pressures, the size of the recirculation zone in water flow as well as the root mean square values of the axial velocity fluctuation in air flow.
Barchilon et al.[10] show that the recirculation zone occurs in cylindrical ducts through measuring mean velocities, the variation of wall static pressures, the size of the recirculation zone in water flow as well as the root mean square values of the axial velocity fluctuation in air flow.
Barchilon et al.[10] show that the recirculation zone occurs in cylindrical ducts through measuring mean velocities, the variation of wall static pressures, the size of the recirculation zone in water flow as well as the root mean square values of the axial velocity fluctuation in air flow.
Razinsky et al.[14] measured the mean velocity, the variation of wall static pressure, root mean square values of the axial velocity fluctuation (turbulent velocity) and Reynolds stress in the water and air flow through changing velocities ratios and diameter ratios when the Craya-Curtet number was below 0.9.
They showed the details of mixing mechanism in confined turbulent jet flow without separating conditions and its transition status to the fully developed confined jet flow.
standing apart; not attached to or supported by anything
They showed the details of mixing mechanism in confined turbulent jet flow without separating conditions and its transition status to the fully developed confined jet flow.
the act of passing from one state or place to the next
They showed the details of mixing mechanism in confined turbulent jet flow without separating conditions and its transition status to the fully developed confined jet flow.
the condition or someone or something at a particular time
They showed the details of mixing mechanism in confined turbulent jet flow without separating conditions and its transition status to the fully developed confined jet flow.
The authors found that the entrainment and mixing depend on the effect of various parameters such as aspect ratio, density ratio, jet Reynolds number and jet location.
The authors found that the entrainment and mixing depend on the effect of various parameters such as aspect ratio, density ratio, jet Reynolds number and jet location.
The authors found that the entrainment and mixing depend on the effect of various parameters such as aspect ratio, density ratio, jet Reynolds number and jet location.
someone who manages property or affairs for someone else
For the variable density jets, Steward and Guruz[17] suggested the non-isothermal Craya-Curtet number (Ctni) from a logical extension of the Craya-Curtet number (Ct) of a uniform density confined jet.
For the variable density jets, Steward and Guruz[17] suggested the non-isothermal Craya-Curtet number (Ctni) from a logical extension of the Craya-Curtet number (Ct) of a uniform density confined jet.
For the variable density jets, Steward and Guruz[17] suggested the non-isothermal Craya-Curtet number (Ctni) from a logical extension of the Craya-Curtet number (Ct) of a uniform density confined jet.
From the physical point of view about equation (2), the dominator of non-isothermal Craya-Curtet number (Ctni) is considered as the availably excess inlet momentum for mixing two flows.
a collection containing a variety of sorts of things
Schefer et al.[18] presented mixture fraction measurement of a turbulent nonreacting propane jet with and without co-flow of air by using laser Rayleigh scattering.
Schefer et al.[18] presented mixture fraction measurement of a turbulent nonreacting propane jet with and without co-flow of air by using laser Rayleigh scattering.
an optical device that produces an intense beam of light
Schefer et al.[18] presented mixture fraction measurement of a turbulent nonreacting propane jet with and without co-flow of air by using laser Rayleigh scattering.
The study of entrainment in turbulent flow is found in the previous papers for many practical situations such as controlling the pattern of flow in combustors.
Pritchard et al.[20] proposed an analytical expression for Rq(entrainment ratio) expressed by in terms of the density ratio(σ), the area ratio(AT/Ao) and friction loss coefficient for the flow in the duct(CL) through using simple momentum and energy balance in eq.(6).
the resistance when a body is moved in contact with another
Pritchard et al.[20] proposed an analytical expression for Rq(entrainment ratio) expressed by in terms of the density ratio(σ), the area ratio(AT/Ao) and friction loss coefficient for the flow in the duct(CL) through using simple momentum and energy balance in eq.(6).
a constant number that serves as a measure of some property
Pritchard et al.[20] proposed an analytical expression for Rq(entrainment ratio) expressed by in terms of the density ratio(σ), the area ratio(AT/Ao) and friction loss coefficient for the flow in the duct(CL) through using simple momentum and energy balance in eq.(6).
having few parts; not complex or complicated or involved
Pritchard et al.[20] proposed an analytical expression for Rq(entrainment ratio) expressed by in terms of the density ratio(σ), the area ratio(AT/Ao) and friction loss coefficient for the flow in the duct(CL) through using simple momentum and energy balance in eq.(6).
Pritchard et al.[20] proposed an analytical expression for Rq(entrainment ratio) expressed by in terms of the density ratio(σ), the area ratio(AT/Ao) and friction loss coefficient for the flow in the duct(CL) through using simple momentum and energy balance in eq.(6).
harmonious arrangement or relation of parts within a whole
Pritchard et al.[20] proposed an analytical expression for Rq(entrainment ratio) expressed by in terms of the density ratio(σ), the area ratio(AT/Ao) and friction loss coefficient for the flow in the duct(CL) through using simple momentum and energy balance in eq.(6).
having the same or nearly the same characteristics
Dahm et al.[21] investigated the mixing and entrainment characteristics experimentally and numerically in the self-similar far field of a steady, axis-symmetrically free turbulent jet flow in the water.
Dahm et al.[21] investigated the mixing and entrainment characteristics experimentally and numerically in the self-similar far field of a steady, axis-symmetrically free turbulent jet flow in the water.
Mohamed et al.[22] suggested the theory of entrainment to study turbulent jet into a stagnant or co-flowing air throughout considering the spreading mixing.
It shows that the entrainment is related to relative velocity difference between the jet and the co-flow as well as the reduction by the co-flow based on the definition of entrainment.
It shows that the entrainment is related to relative velocity difference between the jet and the co-flow as well as the reduction by the co-flow based on the definition of entrainment.
It shows that the entrainment is related to relative velocity difference between the jet and the co-flow as well as the reduction by the co-flow based on the definition of entrainment.
It shows that the entrainment is related to relative velocity difference between the jet and the co-flow as well as the reduction by the co-flow based on the definition of entrainment.
a brief explanation of the meaning of a word or phrase
It shows that the entrainment is related to relative velocity difference between the jet and the co-flow as well as the reduction by the co-flow based on the definition of entrainment.
a structure consisting of an area that has been confined
Kandakure et al.[23] studied the characteristics of turbulent confined jets through checking the effect of enclosure size and the influence of the presence of draft tube.
Kandakure et al.[23] studied the characteristics of turbulent confined jets through checking the effect of enclosure size and the influence of the presence of draft tube.
Kandakure et al.[23] studied the characteristics of turbulent confined jets through checking the effect of enclosure size and the influence of the presence of draft tube.
Singh et al.[24] performed an experimental study of the entrainment and the spread characteristics of confined/semi-confined circular and noncircular confined jets in a circular tube.
It showed that the similarity solutions by Becker et al.[6] are applicable to the circular jet and noncircular jet as well as to the entrainment ratio which generally depends on the diameter of the duct.
It showed that the similarity solutions by Becker et al.[6] are applicable to the circular jet and noncircular jet as well as to the entrainment ratio which generally depends on the diameter of the duct.
Previous research on the fundamental aspects of the mixing such as the concentration and temperature fields to the confined turbulent jets with co-flow is very limited.
This paper represents the applicability of the solutions to the confined jet turbulent flow by conducting numerical and experimental studies of the confined jet as well as proposing a detailed theoretical equation to calculate the amount of entrainment.
relevance by virtue of being relevant to the matter at hand
This paper represents the applicability of the solutions to the confined jet turbulent flow by conducting numerical and experimental studies of the confined jet as well as proposing a detailed theoretical equation to calculate the amount of entrainment.
This paper represents the applicability of the solutions to the confined jet turbulent flow by conducting numerical and experimental studies of the confined jet as well as proposing a detailed theoretical equation to calculate the amount of entrainment.
To measure different velocity range, the pair of absolute pressure transducers (COOPER PTG404 Series) for M>0.3 and four different differential pressure transducers (SETRA C239 series & TESTO) are used below M=0.3.
similar things placed in order or one after another
To measure different velocity range, the pair of absolute pressure transducers (COOPER PTG404 Series) for M>0.3 and four different differential pressure transducers (SETRA C239 series & TESTO) are used below M=0.3.
an intermediate scale value regarded as normal or usual
In this study, all data of the pressure for calculating velocity, temperature and concentration are averaged during 30s after the flows turn to be steady and fully developed mixed with tracer gas before the nozzle.
tending to float on a liquid or rise in air or gas
Since the density of the jet flow and the ambient fluid is different due to different temperature, the buoyant effect is involved in these experiments.
Since the density of the jet flow and the ambient fluid is different due to different temperature, the buoyant effect is involved in these experiments.
For calculating velocity, the pressure data are attained by the Pitot tube connected with the pressure transducer, the temperature is measured by thermocouple and the concentration of NO is measured through sampling tube connected with NO anayalzer (42C High level NOx analyzer).
a relative position or degree of value in a graded group
For calculating velocity, the pressure data are attained by the Pitot tube connected with the pressure transducer, the temperature is measured by thermocouple and the concentration of NO is measured through sampling tube connected with NO anayalzer (42C High level NOx analyzer).
a particular course of action intended to achieve a result
In the beginning, the experimental setup and procedure is validated by measuring the velocity and concentration characteristics of turbulent single jet in the duct for checking the center location of nozzle to make the axis-symmetric jet.
In the beginning, the experimental setup and procedure is validated by measuring the velocity and concentration characteristics of turbulent single jet in the duct for checking the center location of nozzle to make the axis-symmetric jet.
However, it finds that there is the deviation between the data of confined turbulent jet and the data of the free turbulent jet because of the confinement effect from the confined turbulent jet.
The recirculation zone will be caused easily at low non-isothermal Craya-Curtet number because of the high excess momentum at inlet condition between jet and co-flow.
It shows in equation (16) that the axial decay of centerline velocity is expressed as the inverse normalize maximum excess centerline jet velocity by using the characteristic system velocity ( ) defined by Becker et al.[6]. , where (16)
It shows in equation (16) that the axial decay of centerline velocity is expressed as the inverse normalize maximum excess centerline jet velocity by using the characteristic system velocity ( ) defined by Becker et al.[6]. , where (16)
The computed and measured profiles collapse fairly well on a single curve to be represented by a Gaussian function from equation (17), except for the mean scalar fraction at the position far downstream near the near edge(r/rU/2>1).
The computed and measured profiles collapse fairly well on a single curve to be represented by a Gaussian function from equation (17), except for the mean scalar fraction at the position far downstream near the near edge(r/rU/2>1).
The computed and measured profiles collapse fairly well on a single curve to be represented by a Gaussian function from equation (17), except for the mean scalar fraction at the position far downstream near the near edge(r/rU/2>1).
the activity of protecting something from loss or danger
There are difference and scatter in the concentration data at r/rc/2>1 but it can be considered that the normalized NO concentration has self-preservation in jet region for all of test conditions.
We can conclude that the equation (18) can be used for expressing the normalized NO concentration distribution. (a) Ujet=94.56m/s and Uco=0.11m/s (b) Ujet=94.56m/s and Uco=0.4572m/s (c) Ujet=94.56m/s and Uco=0.762m/s (d) Ujet=94.56m/s and Uco=1.11m/s (e) Ujet=157.6m/s and Uco=0.11m/s (f) Ujet=157.6m/s and Uco=0.4572m/s (g) Ujet=157.6m/s and Uco=0.762m/s (h) Ujet=1
The jet width is increasing as moving the normalized axial direction(X/d) because of the characteristics of spreading of the jet though interacting surrounding.
lessen the strength or flavor of a solution or mixture
References [1] Mastorako E., Taylor A. M., Ta and Whitelaw, J. H., Turbulent counterflow flames with reactants diluted by hot products, Joint Meeting of the British and German sections,(1993).
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