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TECHNICAL PAPERS: Heat and Mass Transfer

Three-Dimensional Numerical Calculations of a Jet in an External Cross Flow: Application to Pollutant Dispersion

[+] Author and Article Information
Nejla Mahjoub Said, Hatem Mhiri, Salem El Golli

Laboratoire de Mécanique des fluides et thermique, Ecole Nationale d’Ingénieurs de Monastir, route de Ouardanine 5020, Monastir, Tunisie

Georges Le Palec, Philippe Bournot

Unimeca, 60 rue Joliot-Curie, Technopo⁁le de Cha⁁teau-Gombert, 13453 Marseille Cedex 13, France

J. Heat Transfer 125(3), 510-522 (May 20, 2003) (13 pages) doi:10.1115/1.1560158 History: Received April 24, 2002; Revised November 06, 2002; Online May 20, 2003
Copyright © 2003 by ASME
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References

Kamotani,  Y., and Greber,  I., 1972, “Experiments on a Turbulent Jet in a Cross Flow,” AIAA J., 10, pp 1425–1429.
Fearn,  R., and Weston,  R. P., 1974, “Vorticity Associated With a Jet in a Crossflow,” AIAA J., 12, pp. 1666–1671.
Keffer,  J. F., and Baines,  W. D., 1963, “The Round Turbulent Jet in a Crosswind,” J. Fluid Mech., 15, pp. 481–496.
Moussa,  Z. M., Trischka,  J. W., and Eskinazi,  S., 1977, “The Near Field in the Mixing of a Round Jet With a Cross Stream,” J. Fluid Mech., 15, pp. 481–496.15, 481–496.
Ramsey,  J. W., and Goldstein,  R. J., 1971, “Interaction of a Heated Jet With a Deflecting Stream,” ASME C, J. Heat Transfer , 94, pp. 365–372.
Bergeles,  G., Gosman,  A. D., and Launder,  B. E., 1976, “The Near Field Character of a Jet Discharged Normal to a Main Stream,” ASME C, J. Heat Transfer , 98, p. 373.
Crabb,  D., Durao,  D. F. G., and Whitelaw,  J. H., 1981, “A Round Jet Normal to a Cross Flow,” ASME J. Fluids Eng., 103, pp. 142–152.
Andreopoulos,  J., 1982, “Measurements in a Jet-Pipe Flow Issuing Perpendicularly Into a Cross Stream,” ASME J. Fluids Eng., 104, pp. 493–499.
Andreopoulos,  J., and Rodi,  W., 1984, “Experimental Investigation of Jets in a Crossflow,” J. Fluid Mech., 138, pp. 93–127.
Fric,  T. F., and Roshko,  A., 1994, “Vortical Structure in the Wake of a Transverse Jet,” J. Fluid Mech., 279, pp. 1–47.
Blanchard, J. N., 1996, “Etude d’une interaction d’un jet 2 D avec un écoulement transversal perpendiculaire et confine,” thèse de l’université de Lille.
Boris Papin, Calcul numérique de l’interaction d’un jet et d’un écoulement transversal sur plaque plane, Division Modélisation numérique pour la mécanique des fluides.
Launder,  B. E., and Spalding,  D. B., 1975, “The Numerical Computation of Turbulent Flows,” Comput. Methods Appl. Mech. Eng., 3, pp. 269–282.
Yakhot,  V., Orszag,  S. A., Thengam,  S., Gatki,  T. B., and Speciale,  G., 1992, “Development of Turbulent Models for Shear Flows by a Double Expansion Technique,” Phys. Fluids A, 4(7), pp. 1510–1520.
Chen, Y. S., and Kim, S. W., 1987, “Computation of Turbulent Flows Using an Extended k-ε Turbulence Closure Model,” NASA Contractor Report n° CR-179204.
Roland Schieste, 1993, Modélisation et simulation des écoulements turbulents, Hermès, Paris.
Demuren,  A. O., and Rodi,  W., 1987, “Three Dimensional Numerical Calculations of Flow and Plume Spreading Past Cooling Towers,” J. Heat Transfer , 109, pp. 113–119.
Patankar,  S. V., and Spalding,  D. B., 1972, “A Calculation Procedure for Heat, Mass and Momentum Transfer in Three Dimensional Parabolic Flows,” Int. J. Heat Mass Transf., 15, pp. 1787–1806.

Figures

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Steady flow topology (according to Boris et al. 12)
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Schematic presentation of the grid at the symmetry plane
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Mean ṽ-velocity profiles at the plane of symmetry z/d=0 and R=2.3 at y/d=0.25 with different turbulent models
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Mean ũ-velocity profiles at the plane of symmetry z/d=0 and R=2.3 at y/d=0.75 with different turbulent models
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Mean ũ-velocity profiles at the plane of symmetry z/d=0 for R=0.5
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Centerplane helium mass fraction for R=2.3
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Mean ṽ-velocity profiles
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Mean ṽ-velocity profiles for R=2.3
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Mean ṽ-velocity profiles for R=2.3
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Mean ṽ-velocity profiles for R=2.3
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Mean ũ-velocity profiles for R=2.3
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Mean ũ-velocity profiles for R=2.3
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Mean w̃-velocity profiles for R=2 at y/d=2
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Normal stress profiles vv for R=2.3
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vv-normal-stress profiles for R=2.3
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uv-shear stress profiles for R=2 at z/d=0 Δ experimental 9
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Profiles of the temperature at x/d=8, for R=5
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Cross-sectional contours of the temperature at three planes and R=2
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Temperature contours at the plane of symmetry z/d=0 and R=2
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Profiles of the temperature at y/d=0.25 and z/d=0 for various velocity ratios
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Air mass fraction contours at the plane of symmetry z/d=0 and R=2
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CO2 mass fraction contours at the plane of symmetry z/d=0 and R=2
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Various species mass fraction profiles at y/d=0.25 for R=0.5, in the symmetry plane (z/d=0)
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CO2 mass fraction profiles at y/d=0.25 and z/d=0 for various velocity ratios
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Air mass fraction profiles at y/d=0.25 and z/d=0 for various velocity ratios  
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CO2 mass fraction profiles at y/d=1.35 for R=2
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CO2 mass fraction profiles at x/d=8, for R=5  

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