Simulation of High Pressure Sprays and Radiative Heat Transfer in Internal Combustion Engines


Book Description

High pressure fuel injection is a crucial process that impacts the subsequent steps of mixture preparation, ignition and combustion in diesel or gasoline direct injection engines. Experimental studies have revealed the mixing-controlled and local phase equilibrium characteristics of liquid vaporization in high injection pressure engine sprays. In this study an Equilibrium Phase (EP) spray model is explored. The model is developed based on jet theory and the phase equilibrium assumption, without modeling drop breakup, collision and finite-rate interfacial vaporization processes. The model development is carried out in an advanced version of KIVA-3vr2. The presently proposed EP spray model is validated extensively in simulations of the ECN Spray A, and in an optical diesel engine and in DISI gasoline sprays. The predictions of liquid/vapor penetration, fuel mass fraction distribution, heat release rate and emission formation are in good agreement with experimental data. In addition, good computational efficiency and grid-independency are also seen with the present EP model. The examined operating conditions cover wide ranges that are relevant to IC engines, which are 700-1400 K, 7.6-22.8 kg/m3 for diesel sprays, and 500-900 K, 3-9 kg/m3 for gasoline DISI sprays, respectively. Thermal radiation is another topic of interest in this work since it accounts for an important mechanism of heat transfer in engine combustion. The role of thermal radiation in engine combustion is investigated by implementing the Discrete Ordinate Method (DOM) model and the narrowband model into CFD code together with the EP spray model. Engine simulation results show that radiative heat loss accounts for about 9-18% of the total wall heat loss for operating loads from 4 to 14.5 bar gIMEP. A strong correlation is found between the global equivalence ratio and the fraction of radiative heat loss to total wall heat loss, which even applies in low temperature combustion modes. The participating gases of CO2, H2O and CO are found to be the dominant source of thermal radiation due to their abundancy in high temperature regions. Also, the cooling effect of thermal radiation is shown to have significant impact on the prediction of soot emissions.




Modeling Engine Spray and Combustion Processes


Book Description

The utilization of mathematical models to numerically describe the performance of internal combustion engines is of great significance in the development of new and improved engines. Today, such simulation models can already be viewed as standard tools, and their importance is likely to increase further as available com puter power is expected to increase and the predictive quality of the models is constantly enhanced. This book describes and discusses the most widely used mathematical models for in-cylinder spray and combustion processes, which are the most important subprocesses affecting engine fuel consumption and pollutant emissions. The relevant thermodynamic, fluid dynamic and chemical principles are summarized, and then the application of these principles to the in-cylinder processes is ex plained. Different modeling approaches for the each subprocesses are compared and discussed with respect to the governing model assumptions and simplifica tions. Conclusions are drawn as to which model approach is appropriate for a specific type of problem in the development process of an engine. Hence, this book may serve both as a graduate level textbook for combustion engineering stu dents and as a reference for professionals employed in the field of combustion en gine modeling. The research necessary for this book was carried out during my employment as a postdoctoral scientist at the Institute of Technical Combustion (ITV) at the Uni versity of Hannover, Germany and at the Engine Research Center (ERC) at the University of Wisconsin-Madison, USA.




Radiative Heat Transfer in Turbulent Combustion Systems


Book Description

This introduction reviews why combustion and radiation are important, as well as the technical challenges posed by radiation. Emphasis is on interactions among turbulence, chemistry and radiation (turbulence-chemistry-radiation interactions – TCRI) in Reynolds-averaged and large-eddy simulations. Subsequent chapters cover: chemically reacting turbulent flows; radiation properties, Reynolds transport equation (RTE) solution methods, and TCRI; radiation effects in laminar flames; TCRI in turbulent flames; and high-pressure combustion systems. This Brief presents integrated approach that includes radiation at the outset, rather than as an afterthought. It stands as the most recent developments in physical modeling, numerical algorithms, and applications collected in one monograph.




1D and Multi-D Modeling Techniques for IC Engine Simulation


Book Description

1D and Multi-D Modeling Techniques for IC Engine Simulation provides a description of the most significant and recent achievements in the field of 1D engine simulation models and coupled 1D-3D modeling techniques, including 0D combustion models, quasi-3D methods and some 3D model applications.




High Pressure Combustor Flame and Wall Conjugate Radiative Heat Transfer


Book Description

Efficient aeronautical engines operate at higher pressure ratios and temperature, creating challenges due to higher heat loads. Thermal radiation in aviation has conventionally been treated as correction factors or scaled from experimental data. The complexity of the radiative transfer equation (RTE) leads to computational costly solutions resulting in simplified treatment. The goal of this work is to extend knowledge of non-gray gas radiation modeling to gas-turbine combustor simulations under high-pressure conditions. A one-dimensional temperature solver for combustor liners with thermal barrier coating is developed first, and a non-gray wide-band spectral model for high-pressure conditions is constructed subsequently. Both retrieve spectral properties of combustion gases from high-resolution spectroscopy databases and a Monte Carlo ray tracing solver is used to provide accurate solution of RTE in the gas phase. Frozen-field analysis of a model gas turbine combustor shows heat fluxes concentrated downstream of the main flame brush. Increase of pressure from 1 bar to 40 bar enhances peak radiation loads to the wall by approximately ten folds. A wide-band model is subsequently proposed for gas and soot under pressurized conditions. Improvement in radiative flux prediction is observed when the band definition is carefully chosen around radiative emission peaks, although overall the wide-band model approximates the gray solutions obtained using the MCRT solver closely. Further research is needed to better characterize liner temperature by considering more realistic radiative and convective heat load and TBC parameters. Improvement of the wide-band model is required to better predict the non-gray radiative heat load to the wall.




Radiative Heat Transfer


Book Description

Radiative Heat Transfer, Fourth Edition is a fully updated, revised and practical reference on the basic physics and computational tools scientists and researchers use to solve problems in the broad field of radiative heat transfer. This book is acknowledged as the core reference in the field, providing models, methodologies and calculations essential to solving research problems. It is applicable to a variety of industries, including nuclear, solar and combustion energy, aerospace, chemical and materials processing, as well as environmental, biomedical and nanotechnology fields. Contemporary examples and problems surrounding sustainable energy, materials and process engineering are an essential addition to this edition. - Includes end-of-chapter problems and a solutions manual, providing a structured and coherent reference - Presents many worked examples which have been brought fully up-to-date to reflect the latest research - Details many computer codes, ranging from basic problem solving aids to sophisticated research tools







Droplets and Sprays: Simple Models of Complex Processes


Book Description

This book acts as a guide to simple models that describe some of the complex fluid dynamics, heat/mass transfer and combustion processes in droplets and sprays. Attention is focused mainly on the use of classical hydrodynamics, and a combination of kinetic and hydrodynamic models, to analyse the heating and evaporation of mono- and multi-component droplets. The models were developed for cases when small and large numbers of components are present in droplets. Some of these models are used for the prediction of time to puffing/micro-explosion of composite water/fuel droplets — processes that are widely used in combustion devices to stimulate disintegration of relatively large droplets into smaller ones. The predictions of numerical codes based on these models are validated against experimental results where possible. In most of the models, droplets are assumed to be spherical; some preliminary results of the generalisation of these models to the case of non-spherical droplets, approximating them as spheroids, are presented.




Internal Combustion Processes of Liquid Rocket Engines


Book Description

This book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion.




Modeling Engine Spray and Combustion Processes


Book Description

The utilization of mathematical models to numerically describe the performance of internal combustion engines is of great significance in the development of new and improved engines. Today, such simulation models can already be viewed as standard tools, and their importance is likely to increase further as available com puter power is expected to increase and the predictive quality of the models is constantly enhanced. This book describes and discusses the most widely used mathematical models for in-cylinder spray and combustion processes, which are the most important subprocesses affecting engine fuel consumption and pollutant emissions. The relevant thermodynamic, fluid dynamic and chemical principles are summarized, and then the application of these principles to the in-cylinder processes is ex plained. Different modeling approaches for the each subprocesses are compared and discussed with respect to the governing model assumptions and simplifica tions. Conclusions are drawn as to which model approach is appropriate for a specific type of problem in the development process of an engine. Hence, this book may serve both as a graduate level textbook for combustion engineering stu dents and as a reference for professionals employed in the field of combustion en gine modeling. The research necessary for this book was carried out during my employment as a postdoctoral scientist at the Institute of Technical Combustion (ITV) at the Uni versity of Hannover, Germany and at the Engine Research Center (ERC) at the University of Wisconsin-Madison, USA.