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  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Experiments in fluids 11 (1991), S. 313-324 
    ISSN: 1432-1114
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract The present paper concerns the stagnation flow produced by counter flowing air jets. Little experimental information exists on such flows in spite of their extensive employment in the theoretical treatment of diffusion flames. To remedy this situation, laser-Doppler measurements were performed to quantify the entire flow field. The experiments are described and the results of the velocity measurements presented. Differences between the investigated flow field and the ideal flow field, employed in theoretical studies, are pointed out.
    Type of Medium: Electronic Resource
    Library Location Call Number Volume/Issue/Year Availability
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  • 2
    Electronic Resource
    Electronic Resource
    Springer
    Theoretical and computational fluid dynamics 6 (1994), S. 67-87 
    ISSN: 1432-2250
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics , Physics
    Notes: Abstract Numerical simulation is used in this article to study the structure and dynamics of a spatially growing reactive mixing layer. It is assumed in this analysis that the chemistry is infinitely fast and that it may be modeled by a single-step irreversible reaction. The analysis also relies on thermodiffusive approximation in which the heat released by the chemical reaction does not influence the flow. Calculations performed for a range of values of the global equivalence ratio indicate how the flame evolves as a function of the chemical composition of the two streams. Results of simulations are compared with those of a local model describing the flame elements (the flamelets) that form the flame. Analysis of the fuel consumption rate along the flame sheet indicates that the description of the reactive mixing layer must account for two basic processes. In regions where the reactive surface is isolated, the reaction rate is determined by the local strain rate acting in the plane tangent to the flame. In regions where the flame is rolled-up by the large-scale vortices, it is found that the reaction rate is significantly reduced because the flame elements come close together and interact strongly. Mutual annihilation of the neighboring elements takes place in these circumstances. These two mechanisms, initially proposed by Marble and Broadwell to describe turbulent diffusion flames, are well supported by this simulation. Results of calculations are also used to determine the distributions of mean flame surface density and mean mass fractions. These mean quantities are compared with those determined with a physical model of the turbulent reactive flow. The model is based on a balance equation for the mean flame surface density in combination with a local description in terms of strained flame elements. The agreement obtained indicates that the controlling processes are modeled correctly.
    Type of Medium: Electronic Resource
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  • 3
    Electronic Resource
    Electronic Resource
    Springer
    Flow, turbulence and combustion 65 (2000), S. 205-222 
    ISSN: 1573-1987
    Keywords: LES ; combustion ; instabilities
    Source: Springer Online Journal Archives 1860-2000
    Topics: Mechanical Engineering, Materials Science, Production Engineering, Mining and Metallurgy, Traffic Engineering, Precision Mechanics
    Notes: Abstract This paper describes the first steps in the development of a large eddy simulation (LES) code able to compute combustion instabilities in gas turbines. This code was used to compute the forcing of an experimentally investigated premixed dump combustor. It is shown that the main effect of acoustic waves entering the combustion chamber is to create large vortices and unsteady heat release when these vortices burn. Another effect of waves entering the combustor is to modulate the fuel and air flow rates produced by the feeding lines. In this case the equivalence ratio of the mixture entering the combustor may also vary. This was investigated in a “chemical effect” simulation where the inlet equivalence ratio fluctuates but the total flow rate remains constant. For perturbations from stoichiometric burning, this mechanism was shown to induce less destabilizing effects than the purely aerodynamical mechanism due to vortex formation and combustion. It is shown that the LES methodology developed is able to reproduce the experimentally observed phase shift between acoustic excitation and total reaction rate in the chamber.
    Type of Medium: Electronic Resource
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