The fundamental physics governing wildland fire spread are still largely misunderstood. This thesis was motivated by the need to better understand the role of radiative and convective heat transfer in the ignition and spread of wildland fires. The focus of this work incorporated the use of infrared thermographic imaging techniques to investigate fuel particle response from three different heating sources: convective dominated heating from an air torch, radiative dominated heating from a crib fire, and an advancing flame front in a laboratory wind tunnel test. The series of experiments demonstrated the uniqueness and valuable characteristics of infrared thermography to reveal the hidden nature of heat transfer and combustion aspects which are taking place in the condensed phase of wildland fuelbeds. In addition, infrared thermal image-based temperature history and ignition behavior of engineered cardboard fuel elements subjected to convective and radiative heating supported experimental findings that millimeter diameter pine needles cannot be ignited by radiation alone even under long duration fire generated radiant heating. Finally, fuel characterization using infrared thermography provided a better understanding of the condensed phase fuel pyrolysis and heat transfer mechanisms governing the response of wildland fuel particles to an advancing flame front.

the 18th World Congress The International Federation of Automatic Control, Milano (Italy), August 28 - September 2, 2011

Wildfire processes in Canada are expected to change as a result of climate change. Predictive modeling of wildfire occurrence and susceptibility requires knowledge of ignition expectations and landscape conditions leading to burn. This research examines and quantifies the spatial and temporal patterns of wildfire across Canada with focus on wildfire occurrence and national scale drivers of susceptibility. Baseline ignition expectations and trends are identified and used to create unique fire ignition regimes, assess anthropogenic influence on ignitions, and determine regions with anomalously high ignitions. The aspatial and spatial characteristics of land cover were characterized for pre- and post-fire landscapes. These included land cover composition, configuration, and abiotic covariates. Temporal trends in forest pattern following ignition are examined and national scale drivers of wildfire susceptibility determined. Fire ignition regimes and anomalous ignition regions provide spatially explicit outputs for exploring ignition expectation in Canada. Wildfire was identified to burn mainly in coniferous forests with little fragmentation. Fragmentation increased after wildfire and regeneration of pre-fire forest pattern took 20 years. Additionally, anthropogenic proximity positively influenced ignition expectation, ignition trend, and wildfire susceptibility. This research provides broad scale methods to assess wildfire occurrence and susceptibility across Canada and will facilitate understanding of changing wildfire processes in the future. Additionally, this research highlights the importance of anthropogenic activity on natural fire processes.

The ignition process is a critical consideration for combustion devices. External energy transfer to the combustor is required for ignition in common combustion systems. There are many ways to deposit energy into the flow but a standard method is a spark discharge because it is simple, compact, and reliable. Sparks can be categorized as either inductive or capacitive sparks that use a coil or an electrical resonance circuit with capacitor, respectively, to amplify the voltage. The creation of a successful ignition event depends on the spark energy deposited into the flow, the initial composition, pressure, temperature, turbulence level of flow etc. The deposited energy by the spark into the flow is critical for estimation of initial energy available for ignition of the mixture. Therefore, the electrical characteristics of the sparks were investigated under various flow conditions. Then measurements of deposited energy into the flow were conducted using a very accurate experimental procedure that was developed in this research. The results showed considerable electric energy losses to the electrodes for the relatively long, inductive sparks. However, the short, capacitive spark deposits electric energy into the flow with minimal loss (above 90% deposition efficiency). In addition, the characteristics of inductive spark are affected by flow velocity and by the existence of a flame. However, variations in the flow conditions do not affect the characteristics of the capacitive spark such as voltage-current time trace and energy deposition efficiency. Two ignition systems using above mentioned two spark types were developed. First, the capacitive spark energy was directly deposited into the premixed flow. Most researchers have not concentrated on the early initiation process but on the flame growth. Therefore, the generated kernel formed by the energy deposition was observed and characterized using optical methods, immediately following the spark. In addition, the mixing effect for this ignition kernel with surrounding gas was simulated using a numerical method. Based on the time trace of the OH* chemiluminescence, the reaction starts with the discharge and it is continuous until combustion begins. This means that in the presence of a high density spark in premixed flow, there exists no traditional delay as defined by other researchers for auto ignition. A simple Radical Jet Generator (RJG) was developed that is able to ignite and stabilize a flame in a high-speed flow. The inductive spark initiates the combustion in the RJG chamber. The RJG then injects the partially-burned products carrying large amounts of heat and radicals into a rapidly moving flammable main stream. Then it ignites and stabilizes a flame. The RJG requires low levels of electrical power as long as the flow velocity is relatively low since most of the radicals are produced by the incomplete combustion in its chamber. The importance of radicals was analyzed by RJG experiments and numerical methods. The reaction zone for RJG using a rich mixture was located both inside and outside of the RJG chamber. Therefore, the RJG using a rich mixture performed better in the ignition and stabilization of combustion in the main flow. According to an analysis using the CHEMKIM simulation software combined with the San Diego chemical mechanism, the RJG jet resulting from a rich mixture contains more radicals and intermediates than that produced by a lean mixture for the same sensible enthalpy. In addition, the burned gas contains less radicals and intermediates than the partially burned gas. If the RJG is operating with a high speed main flow, the flow rate through the RJG chamber must be increased to allow the radical jet to penetrate well into the rapid flow due to their higher injection velocity. Unfortunately, this leads to unsteady combustion in the RJG, which results in the pulsation of the radical jet. This reduces the number of radicals injected into the main flow. To investigate this operating condition, special attention was focused on four possible factors: unburned reactant pockets caused by motion of the spark channel, spark frequency, flame propagation speed and ignition delay. It was shown that the unsteadiness is affected by the flame speed and ignition delay because the frequency of pulsation in the chamber is highly dependent on the equivalence ratio. In addition, the interaction between the RJG operation and the combustion dynamics in the main combustor was documented. The acoustic pressure oscillations in the main combustor were suppressed when the RJG jet was turned on because the reaction region is relocated by the operation of the RJG.

Applications of natural gases that contain high levels of hydrogen have become a primary interest in the gas turbine market. For reheat gas turbines, understanding of the ignition delay times of high-hydrogen natural gases is important for two reasons. First, if the ignition delay time is too short, autoignition can occur in the mixer before the primary combustor. Second, the flame in the secondary burner is stabilized by the ignition delay time of the fuel. While the ignition delay times of hydrogen and of the individual hydrocarbons in natural gases can be considered well known, there have been few previous experimental studies into the effects of different levels of hydrogen on the ignition delay times of natural gases at gas turbine conditions. In order to examine the effects of hydrogen content at gas turbine conditions, shock-tube experiments were performed on nine combinations of an L9 matrix. The L9 matrix was developed by varying four factors: natural gas higher-order hydrocarbon content of 0, 18.75, or 37.5%; hydrogen content of the total fuel mixture of 30, 60, or 80%; equivalence ratios of 0.3, 0.5, or 1; and pressures of 1, 10, or 30 atm. Temperatures ranged from 1092 K to 1722 K, and all mixtures were diluted in 90% Ar. Correlations for each combination were developed from the ignition delay times and, using these correlations, a factor sensitivity analysis was performed. It was found that hydrogen played the most significant role in ignition delay time. Pressure was almost as important as hydrogen content, especially as temperature increased. Equivalence ratio was slightly more important than hydrocarbon content of the natural gas, but both were less important than pressure or hydrogen content. Further analysis was performed using ignition delay time calculations for the full matrix of combinations (27 combinations for each natural gas) using a detailed chemical kinetics mechanism. Using these calculations, separate L9 matrices were developed for each natural gas. Correlations from the full matrix and the L9 matrix for each natural gas were found to be almost identical in each case, verifying that a thoughtfully prepared L9 matrix can indeed capture the major effects of an extended matrix.

Metallic materials and oxygen can be a volatile combination when accompanied by ignition mechanisms. Once ignited, metallic materials can readily burn in high pressure oxygen atmospheres, releasing an enormous amount of energy and potentially destroying equipment, space missions and resulting in the loss of life. The potential losses associated with these fires led to research into the conditions under which metal fires propagate. Several organisations, including the American Society for Testing and Materials (ASTM) and the International Organisation for Standardisation (ISO), have published recommended standard test practices with which to assess the relative flammability of metallic materials. These promoted ignition tests, so called because samples are ignited with an overwhelming source of energy, are typically used to examine two important parameters as an indication of a metallic material's flammability: Threshold Pressure (TP) and the Regression Rate of the Melting Interface (RRMI). A material's TP is the minimum pressure at which it burns, therefore, TPs of different materials can be compared to assess which materials are most suited for a range of high pressure applications. The RRMI is a useful measure for ranking materials, particularly if they have the same TP, but can be used as a ranking method irrespective of TP. In addition, it is a crucial parameter to aid in understanding the complex burning process and is one of the few experimental parameters that can be measured. Promoted ignition test standards specify a standard sample geometry to use when performing the test, typically a 3.2 mm diameter cylindrical rod. The recent addition of a 3.2 × 3.2 mm square rod as an optional standard sample geometry raises the issue of how the geometry of a sample affects its flammability. Promoted ignition test results for standard geometries are often applied to assess the flammability risk for the complex geometries of real components within oxygen systems, including regulators, valves, piping etc. Literature shows that sample geometry has a significant effect on material rankings when rankings are based on testing of standard geometries, for example, cylindrical rods, compared to non-standard geometries, for example, sintered filters and meshes. In addition, the RRMI has been shown to be dependent on a sample's cross-sectional area (XA). However, it remains unclear, from a simple heat transfer analysis, why the RRMI is dependent on XA or how the shape of a sample affects its melting rate. These questions are particularly relevant since understanding how sample geometry affects burning contributes to two important research goals: to be able to accurately model and predict the flammability risk of a metallic component without the need for physical testing, and to understand the effects of different sample geometries on their relative flammabilities within the standard tests used. Promoted ignition tests were conducted on iron rods with cylindrical, rectangular and triangular cross sections for a range of XAs. Their RRMIs were measured and analysed using a statistical approach which allowed differences in RRMI to be quantitatively assessed. Statistically significant differences in RRMI were measured for rods with the same XA but of different shape. Furthermore, the magnitude of the difference was dependent on XA. Triangular rods had the fastest RRMIs, followed by rectangular rods and then cylindrical rods. Differences in RRMI based on rod shape are due to heat transfer effects and the dynamic motion of the attached molten mass during the drop cycle. The corners of the rectangular and triangular rods melt faster due to their locally higher Surface Area to Volume ratio (SA/V). This dynamic effect increases the area of contact between the molten mass and the solid rod (solid liquid interface (SLI)) which facilitates increased heat transfer to the rod resulting in a faster RRMI. This finding highlights the importance of the SLI in the heat transfer process. Although the SLI is largely dependent on the XA, the shape of the rod causes subtle changes to the size of the SLI and thus affects heat transfer, burning and observed RRMI. The relationship between rod diameter, test pressure and Extent of Reaction (ER), the proportion of metal that reacts (oxidises) whilst attached to the burning rod, was investigated. During promoted ignition testing of iron rods of varying diameter the detached drops were rapidly quenched by immersion in a water bath. Microanalysis techniques were used to qualitatively assess the ER as a function of pressure and rod diameter. It was found that the pressure dramatically affects ER. High pressure tests resulted in a slag mass consisting of oxide, with no unreacted iron, whereas low pressure tests resulted in a significant fraction of unreacted iron within the slag. This indicates that the ER contributes directly to the observed increase in RRMI with increasing test pressure. At high pressures the ER is not affected by rod diameter, since all available liquid metal reacted, but at low pressures ER is a function of rod diameter, ER decreases as XA increases. This thesis also investigates the analysis of promoted ignition test data through suitable statistical methods. Logistic regression is identified as an appropriate method for modelling binary burn/no-burn test data. The relationship between the reaction probability, defined as the probability that a sample will undergo sustained burning, and pressure, is evaluated for two different data sets. The fits of the logistic regression models are assessed and found to model the available data well. The logistic regression method is contrasted with the confidence levels associated with binary data based on the Bernoulli distribution. It is concluded that a modelling approach is beneficial in providing an overall understanding of the transition between pressures where no burning occurs and pressures where burning is expected.

Homogeneously charged spark ignition (SI) engines are unable to stabilise the combustion in ultra lean mixtures, therefore they operate with a near stoichiometric air-fuel ratio (AFR) at all load points. This produces high engine out NOx and CO emissions with a compromise on fuel consumption. Moreover, stoichiometric operation is needed for effective operation of a three way catalyst, which is not adequate to meet future fuel consumption targets. (For complete abstract open document)

Doctor of Philosophy(PhD) / This body of research uses numerical and experimental investigative techniques to further the understanding of autoignition. Hydrogen/nitrogen and methane/air fuel configurations of turbulent lifted flames in a vitiated coflow burner are used as model flames for this investigation. Characterisation was undertaken to understand the impact of controlling parameters and the overall behaviour of the flames, and to provide a body of data for modelling comparisons. Modelling of the flames was conducted using the PDF-RANS technique with detailed chemistry incorporated using In-situ Adaptive Tabulation (ISAT) within the commercial CFD package, FLUENT 6.2. From these investigations, two numerical indicators for autoignition were developed: convection-reaction balance in the species transport budget at the mean flame base; and the build-up of ignition precursors prior to key ignition species. These indicators were tested in well defined autoignition and premixed flame cases, and subsequently used with the calculated turbulent lifted flames to identify if these are stabilised through autoignition. Based on learnings from the modelling, a quantitative, high-resolution simultaneous imaging experiment was designed to investigate the correlations of an ignition precursor (formaldehyde: CH2O) with a key flame radical (OH) and temperature. Rayleigh scattering was used to measure temperature, while Laser Induced Fluorescence (LIF) was used to measure OH and CH2O concentrations. The high resolution in the Rayleigh imaging permitted the extraction of temperature gradient data, and the product of the OH and CH2O images was shown to be a valid and useful proxy for peak heat release rate in autoigniting and transient flames. The experimental data confirmed the presence of formaldehyde as a precursor for autoignition in methane flames and led to the identification of other indicators. Sequenced images of CH2O, OH and temperature show clearly that formaldehyde exists before OH and peaks when autoignition occurs, as confirmed by images of heat release. The CH2O peaks decrease later while those of OH remain almost unchanged in the reaction zone.

Une des solutions pour diminuer les émissions polluantes émises par un moteur à combustion interne est de réinjecter une partie des gaz d’échappement (Exhaust Gas Recirculation, EGR) à l'admission. Cependant, dans le cas d’une dilution du mélange air-carburant trop importante, la combustion est plus instable voire ne pas s’entretenir. L’ajout d’une faible quantité d’hydrogène a le potentiel de contrer cet effet négatif de forte dilution. C’est dans ce contexte que ce travail de thèse est basé sur une étude détaillée des effets combinés de l’ajout de l’hydrogène et de la dilution dans un moteur à allumage commandé alimenté par du méthane ou de l’iso-octane. Dans la première partie de ce travail, le potentiel de l’ajout de l’hydrogène combiné à la dilution, en termes d’émissions polluantes et de rendement global du moteur, est montré. Dans la deuxième partie, afin de mieux comprendre l’effet de l’hydrogène et de la dilution dans un moteur à combustion interne et leurs influences sur les propriétés fondamentales de la combustion, la vitesse de combustion laminaire, paramètre fondamentale, a été déterminée expérimentalement pour des mélanges isooctane ou méthane avec de l’air contenant différents pourcentages d’hydrogène et de dilution. Des corrélations ont pu ainsi être formulées permettant d’estimer la vitesse fondamentale de combustion laminaire pour ces mélanges. Dans la dernière partie, l’utilisation de deux diagnostics optiques (la chemiluminescence de la flamme et la tomographie par plan laser du front de flamme couplé à la mesure de vitesse par vélocimétrie par imagerie de particules) a permis de quantifier l’effet de l’hydrogène et de la dilution sur la propagation de flamme turbulente dans un moteur à allumage commandé muni d’accès optiques. Nous avons ainsi montré que le la vitesse de combustion laminaire a un effet prépondérant, comparé au nombre de Lewis, sur la vitesse de combustion turbulente dans un moteur à allumage commandé. / Optimization of the intake air-fuel mixture composition is one way to reduce pollutant emissions in Spark-Ignition (SI) engines. This can be achieved by operating with a diluted mixture, i.e by recirculating the exhaust. There are however limitations on the level of dilution that can ensure the smooth running of SI engines since diluting the air-fuel mixture induces an increase in combustion duration and in cyclic variations which impair engine performance. Adding an amount of hydrogen to the fuel can extend the dilution and the lean engine operability limits, which is beneficial in reducing both emission levels and fuel consumption. The objective of this study is to investigate the combined effects of hydrogen addition and nitrogen dilution in an SI engine fuelled with iso-octane or methane. In the first part of this study, we proved that high values of indicated engine efficiency and low values of pollutant emissions can be achieved by combining hydrogen addition and diluted air-fuel mixtures in the case of SI engines. In the second part, we provided experimental values of laminar burning velocity for diluted methane or iso-octane/hydrogen/air mixtures for a better understanding of the hydrogen and dilution effects on the fundamental properties of laminar combustion. New correlations to estimate laminar burning speeds of these mixtures were also presented. In the last part, the effects of hydrogen addition, with and without nitrogen dilution, on the turbulent flame propagation were investigated in an optical SI engine fuelled with iso-octane or methane. This study was done by using two different experimental techniques (direct flame radiation visualization and laser tomography images with Particle Image Velocimetry). The main conclusion is that the laminar burning velocity, rather than the Lewis number, has the dominant effect on the turbulent burning velocity in an SI engine.

Depuis plusieurs années, la diminution des réserves de pétrole incite les différents pays à accroitre leur indépendance énergétique. De plus, diminuer l’impact environnemental de la voiture est devenu l’une des priorités de notre société. En ce sens, les normes Européennes anti-pollution sont devenues plus strictes, tandis que certains polluants sont pointés du doigt pour avoir un impact néfaste sur la santé et l’environnement. Pour répondre à cette double problématique, l’utilisation de biocarburants de type alcools dans les moteurs à allumage commandé est l’une des voies envisagées. Ce virage a déjà été entrepris à petite échelle par l’Union Européenne qui a tout d’abord autorisé l’ajout de 5%, puis de 10% d’éthanol dans l’essence. En plus de l’éthanol déjà commercialisé, le Biobutanol, biocarburant de seconde génération, apparait comme un candidat à fort potentiel pour une utilisation dans les moteurs à allumage commandé. L’objectif de ce travail de thèse est d’étudier le potentiel de l’utilisation de mélanges isooctane/butanol dans les moteurs à allumage commandé, en termes de performances et d’émissions polluantes. De plus, ces résultats sont comparés à ceux de mélanges isooctane/éthanol. Le dégagement de chaleur dans un moteur à allumage commandé est en partie piloté par la vitesse de combustion laminaire. Cette caractéristique a été étudiée de manière expérimentale et numérique pour différentes conditions initiales (pression et richesse) dans une enceinte à volume constant. Puis, une étude sur les premières étapes de la propagation de la combustion a été réalisée dans un moteur monocylindre à accès optique. Ces résultats en moteur ont été corrélés avec les informations laminaires. Enfin, les émissions de polluants réglementés et non-réglementés, ainsi que les performances ont été étudiées dans un moteur monocylindre à allumage commandé. Une baisse de la plupart de ces émissions a été observée avec l’ajout des deux alcools. / For the past few years, the oil stock decrease encourages the different countries to increase their energy independence. Moreover, reducing the environmental impact of transportation became one of the priorities of our society. In this way, European emissions standards are stricter while several pollutants have been identified to have a negative impact on health and the environment. To answer this double problem, the use of alcohols biofuels in spark-ignition engines is one the promising ways. The European Union have already taken a small step in that direction by allowing a maximum of 10% of ethanol into gasoline. As well as ethanol is already marketed, Biobutanol, a 2nd generation biofuel, appears as a serious candidate with a strong potential for a spark-ignition engines use. The objective of this dissertation is to study the potential of the iso-octane/butanol blends use in spark-ignition engines, in terms of performance and pollutants emissions. Moreover, these results are compared to isooctane/ethanol blends. The heat release in spark-ignition engine is piloted for a part by laminar burning velocity. This characteristic was studied experimentally and numerically for different initial conditions (pressure and equivalence ratio) in a constant volume bomb. Then, the early flame kernel growth was studied in a spark-ignition single cylinder engine equipped with optical accesses. Those results were correlated with the results on the laminar burning velocity. Finally, regulated and non-regulated pollutants emissions and engine performance were investigated in a spark-ignition single cylinder engine. A decrease of most pollutant emissions was observed with both alcohols addition.