1990
DOI: 10.1016/0017-9310(90)90007-h
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Structure of turbulent reacting gas jets in liquids at different temperatures and pressures

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Cited by 6 publications
(14 citation statements)
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“…The lithium subcooling effect on the flow structure was examined Chan and Shen (1990) HCl-aqueous NH 3 . The data of Cho et al (1990) were simulated DH=3420 (kJ/kg of HCl), C p = 4.76 (kJ/kg K), density (kg/m 3 ), HCl = 2.3 aq., NH 3 =690 ID = 0.1 m, Height = 0.45 m, nozzle ID = 1 Â 10 À 3 m, nozzle submergence = 0.05 m, orientation = vertical upward LHF+ k-e-g model +cliped Gaussian PDF…”
Section: Discussionmentioning
confidence: 99%
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“…The lithium subcooling effect on the flow structure was examined Chan and Shen (1990) HCl-aqueous NH 3 . The data of Cho et al (1990) were simulated DH=3420 (kJ/kg of HCl), C p = 4.76 (kJ/kg K), density (kg/m 3 ), HCl = 2.3 aq., NH 3 =690 ID = 0.1 m, Height = 0.45 m, nozzle ID = 1 Â 10 À 3 m, nozzle submergence = 0.05 m, orientation = vertical upward LHF+ k-e-g model +cliped Gaussian PDF…”
Section: Discussionmentioning
confidence: 99%
“…The modeling of reaction jets has been undertaken using either locally homogeneous flow (LHF, Chen and Faeth, 1983;Chan and Shen, 1990), two-fluid model (TFM, Zhang et al, 2002) or the multifluid model (MFM, Chan and Abou Ellai, 1991). Chan et al (1988 reported that the plume dimension predictions, using the locally homogeneous flow (LHF) with probability density function (PDF) approach and the k-e-g turbulence model, were reasonable for the reactive jets.…”
Section: Computational Workmentioning
confidence: 99%
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“…The nonlinear equations of imperfect gases, solutes, and solvent of nonideal electrolytic as well as nonelectrolytic solutions were solved by a modified Newton-Raphson iteration scheme using partial molal (or molar) enthalpy, activity coefficient expression, thermodynamic data and chemical potential expressions. 21 The instantaneous scalar thermodynamic properties at each point in the flow correspond to the state reached when injected and ambient fluid at their initial states, having proportions given by the mixture fraction, are adiabatically mixed and brought to thermodynamic equilibrium at the ambient pressure of the flow. Therefore, the scalar thermodynamic properties of the flow were determined, as a function of the mixture fraction (termed as state relationships), by simple adiabatic mixing calculations for given injector exit and ambient conditions and pressure.…”
Section: Equilibrium State Relationshipmentioning
confidence: 99%
“…Computer simulation of liquid metal fuel combustors has recently been adopted as the next possible technique for obtaining detailed information regarding the multiphase submerged flame structure [1][2][3][4][5][6][7][8][9][10][11].…”
Section: List Of Figuresmentioning
confidence: 99%