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Simulation combustion

Four component models were found very difficult or impossible to converge. Models K, M and O are more complicated and have more reaction paths compared to models 1 or N. Whenever the parameter with the highest variance was eliminated in any of these three models, it would revert back to the simpler ones Model I or N. Model N was the only four pseudo-component model that converged. This model also provides an estimate of the HO/LO split. This model together with model 1 were recommended for use in situ combustion simulators (Hanson and Kalogerakis, 1984). Typical results are presented next for model I. [Pg.364]

COSILAB Combustion Simulation Software is a set of commercial software tools for simulating a variety of laminar flames including unstrained, premixed freely propagating flames, unstrained, premixed burner-stabilized flames, strained premixed flames, strained diffusion flames, strained partially premixed flames cylindrical and spherical symmetrical flames. The code can simulate transient spherically expanding and converging flames, droplets and streams of droplets in flames, sprays, tubular flames, combustion and/or evaporation of single spherical drops of liquid fuel, reactions in plug flow and perfectly stirred reactors, and problems of reactive boundary layers, such as open or enclosed jet flames, or flames in a wall boundary layer. The codes were developed from RUN-1DL, described below, and are now maintained and distributed by SoftPredict. Refer to the website http //www.softpredict.com/cms/ softpredict-home.html for more information. [Pg.755]

Using these methods, the elementary reaction steps that define a fuel s overall combustion can be compiled, generating an overall combustion mechanism. Combustion simulation software, like CHEMKIN, takes as input a fuel s combustion mechanism and other system parameters, along with a reactor model, and simulates a complex combustion environment (Fig. 4). For instance, one of CHEMKIN s applications can simulate the behavior of a flame in a given fuel, providing a wealth of information about flame speed, key intermediates, and dominant reactions. Computational fluid dynamics can be combined with detailed chemical kinetic models to also be able to simulate turbulent flames and macroscopic combustion environments. [Pg.90]

Fig. 4 Flow chart for a typical combustion simulation method. Adapted from Reference 35. Fig. 4 Flow chart for a typical combustion simulation method. Adapted from Reference 35.
Leeds University Combustion Simulations Web site. www.chem.leeds.ac.uk/-Combustion/Combustion.html, 2002. [Pg.813]

Zhang, N., EMMS-based Meso-Scale Mass Transfer Model and Its Application to Circulating Fluidized Bed Combustion Simulation, Ph.D. thesis (in Chinese), Institute of Process Engineering, Chinese Academy of Sciences, Beijing (2010). Zhang, J., Ge, W. and Li, J., Chem. Eng. Sci. 60(11), 3091-3099 (2005). [Pg.58]

The third level of combustion simulations is direct numerical simulations (DNS) where the full instantaneous Navier-Stokes equations are solved without any model for turbulent motions all turbulence scales are explicitly determined and their effects on combustion are captured. DNS would predict all time variations of temperature (Fig. 7.4) exactly like a high-resolution sensor would measure them in an experi-... [Pg.240]

For a long time the main topic of research in the area of sensitivity analysis was to find an accurate and effective method for the calculation of local concentration sensitivities. This question now seems to be settled, and the decoupled direct method (ddm) is generally considered the best numerical method. All the main combustion simulation packages such as CHEMKIN, LSENS, RUNIDL and FACSIMILE calculate sensitivities as well as the simulation results and, therefore, many publications contain sensitivity calculations. However, usually very little information is actually deduced from the sensitivity results. It is surprising that the application of principal component analysis is not widespread, since it is a simple postprocessing method which can be used to extract a lot of information from the sensitivities about the structure of the kinetic mechanism. Also, methods for parameter estimation should always be preceded by the principal component analysis of the concentration sensitivity matrix. [Pg.325]

L.J. Clifford, A.M. Mime, T. Tur nyi and D. Boulton, An Induction Parameter Model for Shock-Induced Hydrogen Combustion Simulations, Comb, and Flame (1996) in press. [Pg.436]

World Wide Web files. Combustion Simulations in the Dainton Laboratory at the School of Chemistry (The University of Leeds. http //chem.leeds.ac.uk/Combus-tion/Combustion. html). [Pg.437]

Hudgens, J. W. Workshop on combustion simulation databases for real transportation fuels NIST Gaithersburg, MD (2003). [Pg.164]

Use of Kinetic Models for Solid State Reactions in Combustion Simulations... [Pg.351]

A logical next step is to incorporate these numerical models into combustion simulations. Ultimately, though, it will be necessary to develop new kinetic paradigms for condensed phase reaction kinetics that are firmly grounded in the underlying molecular properties. [Pg.356]

For future combustion simulations, we have listed in Table 1 the molecular parameters and heats of formation of key species involved in the reactions studied. Table 2 summarizes the predicted rate constants calculated for varying experimental conditions covering those relevant to the stratosphere 03-destruction and AP combustion chemistry for applications by scientists in both research communities. [Pg.437]

For practical reasons, the number of LOS measurements is finite, and the tomographic reconstruction problem is ill-posed. Two reconstruction methods have been developed for cases where optical access is restricted, and the number of measurement LOSs is limited. One method, adaptive FDDI, requires 100 or more LOSs [1-3], while the other method. Tomographic Reconstruction via a Karhunen-Loeve Basis, requires far fewer [4, 5]. Because it requires very few LOSs, the authors believe that this latter method has potential for use in sensing for feedback control of combustion systems where optical access is limited however, it requires considerable a priori information in the form of a set of expected distributions, the training set. This set is analyzed via POD to yield a set of basis functions, the Karhunen-Loeve eigenfunctions, that are used for reconstruction. These training sets could come from measurements on prototype equipment or from computational combustion simulations. [Pg.10]

Experimental and computational aeroacoustics and emissions of modern swirl combustor flows are underway. Preliminary measurements of turbulent non-premixed flame sound highlight the influence of combustion as a sound source. Particle Image Velocimetry measurements in swirl combustors reveal the influence of heat release and its effect on the complex spatial structures that are present. Acoustic measurements in confined turbulent jets are used to better understand sound sources in such flows. Computational aeroacoustics studies of unconfined and confined flows and flames have allowed acoustic source identification. Preliminary LES of diffuser and swirl combustor flowfields serve as benchmarks for future combustion simulations. [Pg.221]

Suresh K. Aggarwal (combustion simulations, renewable fuels). University of Illinois at Chicago, IE... [Pg.320]

Today, CAD/CAM simulations as a tool to estimate performanee of various systems, reduce costs and testing time is taken into consideration. In this study speeified engine and its components have been simulated by GT-POWER software carefully. Modeling of software is based on fluid mechanics laws, thermodynamic laws, mass conservation law, equilibrium reactions, and chemical kinetics. In particular, combustion simulation of this software is based on one... [Pg.40]

Hughes, K. Turanyi, T. Pilling, M. (2001). The Leeds methane oxidation mechanism, ver 1.5, In Combustion Simulation, September 2011, Available from http //garfield.chem.elte.hu/Combustion/ methane.htm... [Pg.387]

Clifford, L.J., Milne, A.M., Turanyi, T., Boulton, D. An induction parameter model for shock-induced hydrogen combustion simulations. Combust. Flame 113, 106-118 (1998)... [Pg.295]

Liang, L., Stevens, J.G., Raman, S., Farrell, J.T. The use of dynamic adaptive chemistry in combustion simulation of gasoline surrogate fuels. Combust. Flame 156, 1493-1502 (2009b) Liao, J.C., Lightfoot, E.N. Lumping analysis of biochemical reaction systems with time scale separation. Biotechnol. Bioeng. 31, 869-879 (1988)... [Pg.301]

Oluwole, O.O., Shi, Y., Wong, H.W., Great, W.H. An exact-steady-state adaptive chemistry method for combustion simulations cmnbining the efficiency of reduced models and the accuracy of the full model. Combust. Flame 159, 2352-2362 (2012)... [Pg.305]

Wang, H., Yao, M., Reitz, R.D. Development of a reduced primary reference fuel mechanism for internal combustion engine combustion simulations. Energy Fuels 27, 7843-7853 (2013) Wamatz, J. Resolution of gas phase and surface combustion chemistry into elementary reactions. Proc. Combust. Inst. 24, 553-579 (1992)... [Pg.311]


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See also in sourсe #XX -- [ Pg.2 , Pg.227 , Pg.351 , Pg.356 , Pg.357 , Pg.358 , Pg.359 , Pg.360 , Pg.361 , Pg.362 , Pg.363 , Pg.364 , Pg.365 , Pg.366 , Pg.367 , Pg.368 ]




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