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  • 1
    Book
    Book
    London u.a. :Academic Press,
    Title: Turbulent reacting flows
    Contributer: Libby, Paul A. , Williams, Forman A.
    Publisher: London u.a. :Academic Press,
    Year of publication: 1994
    Pages: 647 S.
    Series Statement: Combustion treatise
    Type of Medium: Book
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  • 2
    Electronic Resource
    Electronic Resource
    New York, NY : American Institute of Physics (AIP)
    Physics of Fluids 5 (1993), S. 203-216 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: The flow arising from two, closely spaced turbulent jets flowing counter to one another is analyzed for both two-dimensional and axisymmetric configurations. By closely spaced it is indicated that the diameter of the jets is large compared to their separation distance. Two parameters, one a measure of the integral scale of the turbulence compared with half the separation distance of the jets, and a second, a measure of the intensity of the turbulence issuing from the jets, are assumed small and form the basis of an asymptotic analysis. As a consequence, the mean velocity components are given by the mean Euler equations, except in a thin layer that is centered about the plane containing either the stagnation line or point and within which discontinuities in the flow from each jet are adjusted. Thus, outside of this layer, the turbulence characteristics in a known mean velocity field are determined, in the present study, in terms of a Reynolds stress description. The rate of strain field associated with the stagnating flow results in anisotropy of the turbulence as the plane containing the stagnation line or point is approached. Differences in the mean velocities in two-dimensional and axisymmetric configurations result in significant differences in the evolution of the gradient of the Reynolds shear stress from the exit planes of the jets and thus in the thin layer at the stagnation plane. For two-dimensional flows, the velocity characteristics in the thin layer satisfy to lowest order in an expansion parameter the requisite symmetry conditions, whereas this is not the case for axisymmetric flows. The temperature in the two streams is assumed to be slightly different but uniform so that there is also a thermal layer at the stagnation plane. Comparison is made with the applicable experimental data for the mean velocity and the turbulence intensities with good and reasonable agreement, respectively.
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    New York, NY : American Institute of Physics (AIP)
    Physics of Fluids 5 (1993), S. 2301-2303 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: Experimental data on the mean axial velocity and the intensity of the radial and axial velocity components on the axis of counterflowing turbulent streams are compared with a previously published Reynolds stress theory. Agreement is found to be satisfactory.
    Type of Medium: Electronic Resource
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  • 4
    Electronic Resource
    Electronic Resource
    New York, NY : American Institute of Physics (AIP)
    Physics of Fluids 4 (1992), S. 391-408 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: The characteristics of isenthalpic planar premixed flames in counterflowing streams involving high Reynolds numbers and either corotating or counter-rotating swirl of large magnitudes are analyzed. The method of activation energy asymptotics is applied to a one-step Arrhenius reaction with small departures from unity Lewis numbers. Density changes resulting from heat release are fully taken into account. High swirl is shown to lead to three stagnation points and regions of radial inflow in agreement with experiment. It is shown that the character of the viscous regions containing the flames and their extinction behavior are significantly influenced by swirl for strong rates of rotation. The present analysis shows that the resonances found in an earlier inviscid calculation are not physically realizable and accounts for the reversal of the lean flammability limit with rotation rate found experimentally.
    Type of Medium: Electronic Resource
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  • 5
    Electronic Resource
    Electronic Resource
    New York, NY : American Institute of Physics (AIP)
    Physics of Fluids 2 (1990), S. 1213-1223 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: The characteristics of isenthalpic planar premixed flames in counterflowing, high Reynolds number streams with counter- and corotating swirl are analyzed by activation energy asymptotics for a one-step Arrhenius reaction with small departures from unity Lewis numbers. Density changes resulting from heat release are fully taken into account. For moderate rates of rotation, the situation considered in the present study, there is only one stagnation plane that is coincident with the plane of symmetry separating the inviscid outer flows and that involves a viscous layer with an embedded flame in some circumstances. The analysis of a flame in the viscous layer is relevant to the experimentally observed variation of the lean flammability limit with the rotation rate. Comparison with the existing experimental data is carried out.
    Type of Medium: Electronic Resource
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  • 6
    Electronic Resource
    Electronic Resource
    New York, NY : American Institute of Physics (AIP)
    Physics of Fluids 2 (1990), S. 1281-1284 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: The forces on droplets in Poiseuille flow in the Reynolds number range from 0.7 to 27 are determined experimentally. It is found that droplets migrate toward the centerline and experience drag considerably in excess of that prevailing in uniform flow. Rough correlations for the drag and lift coefficients as functions of the Reynolds number and a parameter characterizing the flow nonuniformity are developed.
    Type of Medium: Electronic Resource
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  • 7
    Electronic Resource
    Electronic Resource
    [S.l.] : American Institute of Physics (AIP)
    Physics of Fluids 6 (1994), S. 1805-1819 
    ISSN: 1089-7666
    Source: AIP Digital Archive
    Topics: Physics
    Notes: The flow arising from an axisymmetric turbulent jet with an exit plane in close proximity to the wall against which it impinges is analyzed. The reciprocal of a Reynolds number based on the kinematic viscosity adds here to the two parameters identified in Part I [Phys. Fluids A 5, 203 (1993)] as determining the flow characteristics of two opposed jets, namely the ratio of the turbulence scale to the separation of the jet exit from the wall and the ratio of the turbulence intensity to the mean exit velocity. With all three of these parameters suitably small there is indicated an asymptotic analysis which describes separately the flow in three distinct regions. The temperature of the impinging fluid is assumed to be slightly different from that of the wall so that the mean velocity components, the mean temperature, and the various Reynolds stresses and fluxes vary within a thin wall layer which consists of a viscous sublayer and a turbulent shear layer. When the Reynolds number is suitably high, the sublayer accounts for all of the change in the mean radial velocity and in the mean temperature. The analysis of the turbulence external to the wall layer is compared with experimental data on a turbulent jet impinging on a wall. Agreement with respect to the mean axial velocity and the intensities of the axial and radial velocity components is quite satisfactory. Comparison is made with experimental data on heat transfer to the wall; the predicted dependence of Nusselt number on Reynolds number is confirmed.
    Type of Medium: Electronic Resource
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  • 8
    Electronic Resource
    Electronic Resource
    Springer
    Zeitschrift für angewandte Mathematik und Physik 20 (1969), S. 619-627 
    ISSN: 1420-9039
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mathematics , Physics
    Notes: Zusammenfassung Es wird die Grenzschicht an einem abgestumpften Keil mit Hilfe der Görtlerschen Reihe berechnet. Man findet, von der Staupunkt-Grenzschicht ausgehend, eine asymptotische Annäherung an die Grenzschichten von Falkner und Skan; die asymptotische Lösung wird mit Hilfe der Reihe sehr befriedigend dargestellt, besonders nach Anwendung von verschiedenen Methoden zur Verbesserung der Konvergenz. Zudem wird die Annäherung an die Lösung im Unendlichen analytisch untersucht, wobei sogenannte asymptotische Eigenfunktionen auftreten. Die rechnerisch ausgewertete Lösung für einen Keil mit rechteckigem Öffnungswinkel kann als Vergleichsfall zur Beurteilung von numerischen Methoden benützt werden.
    Type of Medium: Electronic Resource
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