Relevant bibliographies by topics / Reacting Mixing Layer

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Academic literature on the topic 'Reacting Mixing Layer'

Author: Grafiati
Published: 4 June 2021
Last updated: 6 September 2023

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Journal articles on the topic "Reacting Mixing Layer"

1

Koochesfahani, M. M., and P. E. Dimotakis. "Mixing and chemical reactions in a turbulent liquid mixing layer." Journal of Fluid Mechanics 170 (September 1986): 83–112. http://dx.doi.org/10.1017/s0022112086000812.

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An experimental investigation of entrainment and mixing in reacting and non-reacting turbulent mixing layers at large Schmidt number is presented. In non-reacting cases, a passive scalar is used to measure the probability density function (p.d.f.) of the composition field. Chemically reacting experiments employ a diffusion-limited acid–base reaction to directly measure the extent of molecular mixing. The measurements make use of laser-induced fluorescence diagnostics and high-speed, real-time digital image-acquisition techniques.Our results show that the vortical structures in the mixing layer initially roll-up with a large excess of fluid from the high-speed stream entrapped in the cores. During the mixing transition, not only does the amount of mixed fluid increase, but its composition also changes. It is found that the range of compositions of the mixed fluid, above the mixing transition and also throughout the transition region, is essentially uniform across the entire transverse extent of the layer. Our measurements indicate that the probability of finding unmixed fluid in the centre of the layer, above the mixing transition, can be as high as 0.45. In addition, the mean concentration of mixed fluid across the layer is found to be approximately constant at a value corresponding to the entrainment ratio. Comparisons with gas-phase data show that the normalized amount of chemical product formed in the liquid layer, at high Reynolds number, is 50% less than the corresponding quantity measured in the gas-phase case. We therefore conclude that Schmidt number plays a role in turbulent mixing of high-Reynolds-number flows.
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Bilger, R. W., L. R. Saetran, and L. V. Krishnamoorthy. "Reaction in a scalar mixing layer." Journal of Fluid Mechanics 233 (December 1991): 211–42. http://dx.doi.org/10.1017/s0022112091000460.

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Reaction in a scalar mixing layer in grid-generated turbulence is studied experimentally by doping half of the flow with nitric oxide and the other half with ozone. The flow conditions and concentrations are such that the chemical reaction is passive and the flow and chemical timescales are of the same order. Conserved scalar theory for such flows is outlined and further developed; it is used as a basis for presentation of the experimental results. Continuous measurements of concentration are limited in their spatial and temporal resolution but capture sufficient of their spectra for adequate second-order correlations to be made. Two components of velocity have been measured simultaneously with hot-wire anemometry. Conserved scalar mixing results, deduced from reacting and non-reacting measurements of concentration, show the independence of concentration level and concentration ratio expected for passive reacting flow. The results are subject to several limitations due to the necessary experimental compromises, but they agree generally with measurements made in thermal mixing layers. Reactive scalar statistics are consistent with the realizability constraints obtainable from conserved scalar theory where such constraints apply, and otherwise are generally found to lie between the conserved scalar theory limits for frozen and very fast chemistry. It is suggested that Toor's (1969) closure for the mean chemical reaction rate could be improved by interpolating between the frozen and equilibrium values for the covariance. The turbulent fluxes of the reactive scalars are found to approximately obey the gradient model but the value of the diffusivity is found to depend on the Damköhler number.
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MILLER, M. F., C. T. BOWMAN, and M. G. MUNGAL. "An experimental investigation of the effects of compressibility on a turbulent reacting mixing layer." Journal of Fluid Mechanics 356 (February 10, 1998): 25–64. http://dx.doi.org/10.1017/s002211209700791x.

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Experiments were conducted to investigate the effect of compressibility on turbulent reacting mixing layers with moderate heat release. Side- and plan-view visualizations of the reacting mixing layers, which were formed between a high-speed high-temperature vitiated-air stream and a low-speed ambient-temperature hydrogen stream, were obtained using a combined OH/acetone planar laser-induced fluorescence imaging technique. The instantaneous images of OH provide two-dimensional maps of the regions of combustion, and similar images of acetone, which was seeded into the fuel stream, provide maps of the regions of unburned fuel. Two low-compressibility (Mc=0.32, 0.35) reacting mixing layers with differing density ratios and one high-compressibility (Mc=0.70) reacting mixing layer were studied. Higher average acetone signals were measured in the compressible mixing layer than in its low-compressibility counterpart (i.e. same density ratio), indicating a lower entrainment ratio. Additionally, the compressible mixing layer had slightly wider regions of OH and 50% higher OH signals, which was an unexpected result since lowering the entrainment ratio had the opposite effect at low compressibilities. The large-scale structural changes induced by compressibility are believed to be primarily responsible for the difference in the behaviour of the high- and low-compressibility reacting mixing layers. It is proposed that the coexistence of broad regions of OH and high acetone signals is a manifestation of a more biased distribution of mixture compositions in the compressible mixing layer. Other mechanisms through which compressibility can affect the combustion are discussed.
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Shin, D. S., and J. H. Ferziger. "Linear stability of the reacting mixing layer." AIAA Journal 29, no. 10 (1991): 1634–42. http://dx.doi.org/10.2514/3.10785.

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MILLER, R. S., C. K. MADNIA, and P. GIVI. "Structure of a Turbulent Reacting Mixing Layer." Combustion Science and Technology 99, no. 1-3 (1994): 1–36. http://dx.doi.org/10.1080/00102209408935423.

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Jianqiang, Chen, and Zhuang Fenggan. "Numerical simulation of supersonic reacting mixing layer." Acta Mechanica Sinica 13, no. 2 (1997): 97–105. http://dx.doi.org/10.1007/bf02487915.

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NAGATA, KOUJI, and SATORU KOMORI. "The effects of unstable stratification and mean shear on the chemical reaction in grid turbulence." Journal of Fluid Mechanics 408 (April 10, 2000): 39–52. http://dx.doi.org/10.1017/s0022112099007594.

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The effects of unstable thermal stratification and mean shear on chemical reaction and turbulent mixing were experimentally investigated in reacting and non-reacting liquid mixing-layer flows downstream of a turbulence-generating grid. Experiments were carried out under three conditions: unsheared neutrally stratified, unsheared unstably stratified and sheared neutrally stratified. Instantaneous velocity and concentration were simultaneously measured using the combination of a laser-Doppler velocimeter and a laser-induced fluorescence technique. The results show that the turbulent mixing is enhanced at both large and small scales by buoyancy under unstably stratified conditions and therefore the chemical reaction is strongly promoted. The mean shear acts to enhance the turbulent mixing mainly at large scales. However, the chemical reaction rate in the sheared flow is not as large as in the unstably stratified case with the same turbulence level, since the mixing at small scales in the sheared neutrally stratified flow is weaker than that in the unsheared unstably stratified flow. The unstable stratification is regarded as a better tool to attain unsheared mixing since the shearing stress acting on the fluid is much weaker in the unstably stratified flow than in the sheared flow.
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Jahanbakhshi, Reza, and Cyrus K. Madnia. "The effect of heat release on the entrainment in a turbulent mixing layer." Journal of Fluid Mechanics 844 (April 3, 2018): 92–126. http://dx.doi.org/10.1017/jfm.2018.122.

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Direct numerical simulations of a temporally evolving compressible reacting mixing layer have been performed to study the entrainment of the irrotational flow into the turbulent region across the turbulent/non-turbulent interface (TNTI). In order to study the effects of heat release and interaction of the flame with the TNTI on turbulence several cases with different heat release levels, $Q$, and stoichiometric mixture fractions are chosen for the simulations with the highest opted value for $Q$ corresponding to hydrogen combustion in air. The combustion is mimicked by a one-step irreversible global reaction, and infinitely fast chemistry approximation is used to compute the species mass fractions. Entrainment is studied via two mechanisms: nibbling, considered as the vorticity transport across the TNTI, and engulfment, the drawing of the pockets of the outside irrotational fluid into the turbulent region. As the level of heat release increases, the total entrained mass flow rate into the mixing layer decreases. In a reacting mixing layer by increasing the heat release rate, the mass flow rate due to nibbling is shown to decrease mostly due to a reduction of the local entrainment velocity, while the surface area of the TNTI does not change significantly. It is also observed that nibbling is a viscous dominated mechanism in non-reacting flows, whereas it is mostly carried out by inviscid terms in reacting flows with high level of heat release. The contribution of the engulfment to entrainment is small for the non-reacting mixing layers, while mass flow rate due to engulfment can constitute close to 40 % of the total entrainment in reacting cases. This increase is primarily related to a decrease of entrained mass flow rate due to nibbling, while the entrained mass flow rate due to engulfment does not change significantly in reacting cases. It is shown that the total entrained mass flow rate in reacting and non-reacting compressible mixing layers can be estimated from an expression containing the convective Mach number and the density change due to heat release.
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Gu, Jin Liang, Huan Hao Zhang, Zhi Hua Chen, and Xiao Hai Jiang. "Numerical Simulation of the Supersonic Planar Mixing Layer." Advanced Materials Research 347-353 (October 2011): 922–26. http://dx.doi.org/10.4028/www.scientific.net/amr.347-353.922.

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Large eddy simulation (LES) has been used to simulate both non-reacting and reacting supersonic planar mixing layers at convective Mach number Mc=0.3. The different eddy characteristics of two cases have been visualized and discussed based on our calculated results, and the differences of mixing layer structures have also been shown, which can provide some important guide for future relative engineering design.
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Mcmurtry, P. A., J. J. Riley, and R. W. Metcalfe. "Effects of heat release on the large-scale structure in turbulent mixing layers." Journal of Fluid Mechanics 199 (February 1989): 297–332. http://dx.doi.org/10.1017/s002211208900039x.

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The effects of chemical heat release on the large-scale structure in a chemically reacting, turbulent mixing layer are investigated using direct numerical simulations. Three-dimensional, time-dependent simulations are performed for a binary, single-step chemical reaction occurring across a temporally developing turbulent mixing layer. It is found that moderate heat release slows the development of the large-scale structures and shifts their wavelengths to larger scales. The resulting entrainment of reactants is reduced, decreasing the overall chemical product formation rate. The simulation results are interpreted in terms of turbulence energetics, vorticity dynamics, and stability theory. The baroclinic torque and thermal expansion in the mixing layer produce changes in the flame vortex structure that result in more diffuse vortices than in the constant-density case, resulting in lower rotation rates of the large-scale structures. Previously unexplained anomalies observed in the mean velocity profiles of reacting jets and mixing layers are shown to result from vorticity generation by baroclinic torques.
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Dissertations / Theses on the topic "Reacting Mixing Layer"

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Veynante, Denis. "Etude numérique et expérimentale d'une zone de mélange réactive." Châtenay-Malabry, Ecole centrale de Paris, 1985. http://www.theses.fr/1986ECAP0033.

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Etude expérimentale d'une couche de mélange bidimensionnelle entre deux écoulements liquides, parallèles, de vitesses différentes et éventuellement réactifs (réaction acide-base) par visualisation et anémométrie laser. Les équations dynamiques sont établies dans le cas des approximations classiques de la couche limite bidimensionnelle; on aborde trois types de fermeture: écoulement laminaire, modèle de la longueur de mélange de Prandtl, modèle de turbulence à deux équations de Saffman. La réaction chimique est représentée à l'aide du modèle de la flamme cohérente de Marble et Broadwell
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Mathey, Fabrice. "Ecoulements cisaillés réactifs : étude par modélisation sous-maille du mélange et simulation numérique des grandes échelles." Université Joseph Fourier (Grenoble), 1997. http://www.theses.fr/1997GRE10215.

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Le formalisme de la simulation des grandes echelles (les) pour l'etude des ecoulements turbulents est presente. Des tests, en configuration de turbulence homogene isotrope et de couche de melange temporelle, mettent en evidence le comportement des differents modeles de viscosite turbulente vis-a-vis de la dissipation generee par les correcteurs de flux du schema ppm. Une solution est proposee permettant d'eviter une dissipation numerique trop importante pour les ecoulements en turbulence developpee et d'eviter le developpement d'instabilites numeriques dues aux conditions initiales. Les modeles de melange sous-maille specifiques aux ecoulements reactifs sont ensuite presentes. Deux approches sont en particulier retenues. Une approche stochastique, permettant de reconstruire jusqu'aux plus petites echelles l'evolution d'un champ de scalaire : le lem (linear eddy model). On montre que cette approche permet en particulier de reproduire des lois d'echelles observees dans les experiences et s'ecartant des theories classiques du melange. Puis une approche probabiliste ou la structure du champ a petite echelle est presumee a partir d'une fonction de densite de probabilite. Cette derniere approche necessite la modelisation de la variance sous-maille de la fraction de melange. Pour cela, une nouvelle modelisation est presentee, permettant des simulations les sans parametres ajustable. Ce modele est valide par des tests a priori a partir de simulations lem a grands nombres de reynolds, puis par des simulations de couche de melange temporelle reactive. Dans ce dernier cas, les resultats obtenus lors des phases de transition et de turbulence developpees sont compares aux experiences de la litterature. On montre que les quantites de produits sont correctement representees par le modele sous-maille de melange. Ces simulations permettent de mettre en evidence les mecanismes de la transition de melange et le role des tourbillons longitudinaux.
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Pit, Fabienne. "Modélisation du mélange pour la simulation d'écoulements réactifs turbulents : essais de modèles eulériens lagrangiens." Rouen, 1993. http://www.theses.fr/1993ROUE5020.

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Ce travail porte sur la modélisation et la simulation d'écoulements réactifs turbulents à chimie non infiniment rapide par une fonction densité de probabilité conjointe. La résolution de l'équation d'évolution temporelle de la PDF conjointe analytiquement ou numériquement est très complexe. En fait, le problème est simplifié en intégrant cette équation dans l'espace des vitesses. On obtient ainsi une approche hybride probabiliste eulérienne lagrangienne. Une méthode de Monte-Carlo est utilisée ensuite, pour simuler cette équation. Dans cette équation, le phénomène de mélange a petite échelle doit être représenté par un modèle. La comparaison d'un nouveau modèle de mélange avec des modèles classiques d'échange avec la moyenne a été faite dans le cas d'une couche de mélange thermique et dans le cas d'une couche de mélange réactive. Les résultats des calculs sont encourageants. La possibilité de l'appliquer à des configurations industrielles complexes 2D axisymétrique (le bluff-body) et 3D (chambre de combustion dextre) est démontrée
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Hartsfield, Carl Rex. "Reactive shear layer mixing and growth rate effects on afterburning properties for axisymetric rocket engine plumes." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://library.nps.navy.mil/uhtbin/hyperion/06Sep%5FHartsfield.pdf.

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Dissertation (Ph.D. in Astronautical Engineering)--Naval Postgraduate School, September 2006.<br>Thesis Advisor(s): Christopher M. Brophy. "September 2006." Includes bibliographical references (p.153-157). Also available in print.
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Siklawi, Charbel. "Large eddy simulation (2D) using vortex-in-cell and filtered density function for isothermally reacting and thermally stratified mixing layers." Thesis, University of Ottawa (Canada), 2009. http://hdl.handle.net/10393/28157.

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A large eddy simulation based on the filtered vorticity transport equation has been coupled with the filtered mass weighted density function transport equation. The filtered vorticity transport has been formulated using the diffusion-velocity method and then solved using the vortex-in-cell scheme in conjunction with both Smagorinsky and dynamic eddy viscosity subgrid scale models for an anisotropic flow. The transport equation for filtered mass weighted density function is solved using the Lagrangian Monte-Carlo method. The methodology has been tested on both chemically reacting with no heat release and thermally stratified spatially growing mixing layers. It is shown that mixing has a greater effect on scalar field within the vortex structure as compared to the braid regions. Also for high Damkohler number (Da), the reaction zones are mainly limited to the thin reacting interfacial zones, i.e. the contact zone between the reactants, whereas for low Da, the reacting zones are spread as reacting pockets within the vortex structure. The effect of vorticity-temperature interaction, i.e., the volumetric expansion and baroclinic vorticity generation, on the flow field is also investigated by mixing a cold and a hot stream with temperature differences of 0, 5, 10, 30 and 50&deg;K. The mixing layer is destabilized earlier and the pairing of vortical structures is reduced as temperature difference is increased. The characteristics of the flow field, i.e. the vorticity contours, the mean velocity, root-mean-square velocity fluctuations and negative cross-stream correlations are discussed. Also, the characteristics of the scalar field, i.e. the mean scalar profiles, root-mean-square scalar fluctuations profiles and filtered probability density function are presented.
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Thurlow, Meghan Elizabeth. "Free Radicals and Reactive Intermediates in the Boundary Layer: Development and Deployment of Solid-State Laser Based Instrumentation to Measure Part per Trillion Mixing Ratios of Iodine Monoxide and Glyoxal In Situ." Thesis, Harvard University, 2012. http://dissertations.umi.com/gsas.harvard:10668.

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Advances in spectroscopic measurement techniques enabling highly accurate measurements of trace gases in the atmosphere are critical for furthering our understanding of the chemical processes that impact both climate and human health. This dissertation presents the development and deployment of laser-based instruments for measuring parts per trillion (pptv) concentrations of iodine monoxide and glyoxal. Iodine, which is primarily released from oceanic sources, is highly reactive in the atmosphere. Despite its trace concentrations, iodine plays a potentially important role in ozone destruction, the catalysis of mercury deposition, and the formation of marine clouds. An in situ instrument to detect iodine monoxide (IO) using laser-induced fluorescence was developed and then validated during a deployment to the Shoals Marine Laboratory (Appledore Island, ME) in August and September 2011. Mixing ratios up to 10 pptv of IO were observed with a strong tidal dependence. The instrumental detection limit \((3\sigma)\) of 0.36 pptv in 1 minute is indicative of unprecedented sensitivity. Glyoxal, the smallest alpha-dicarbonyl, serves as an atmospheric tracer of both the oxidation of biogenic volatile organic compounds in forest environments as well as secondary organic aerosol. Modeling studies indicate that production of glyoxal on a global scale is driven primarily by biogenic emissions, specifically emissions of isoprene. However, measurements of glyoxal in environments where isoprene dominates its production are limited. An instrument to detect glyoxal in situ by laser-induced phosphorescence was developed. The 3σ limit of detection of this instrument was 3.9 pptv in 1 minute. During July and August 2009, gas-phase measurements of glyoxal were made during the Community Atmosphere-Biosphere Interactions Experiment at the PROPHET tower in an isoprene-dominated forest site in northern Michigan. Additional measurements made throughout the campaign have been used to constrain a box model using the Master Chemical Mechanism. The model over-predicts glyoxal relative to the observed mixing ratios. Theoretically predicted reaction pathways implemented in many isoprene oxidation schemes exacerbate this disagreement.<br>Chemistry and Chemical Biology
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Stoukov, Alexei. "Etude numérique de la couche de mélange réactive supersonique." Rouen, 1996. http://www.theses.fr/1996ROUES013.

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L'objet de ce travail concerne l'analyse et la simulation numérique de la couche de mélange supersonique réactive instationnaire. Le premier chapitre présente le contexte général de l'étude et les problèmes spécifiques abordés. Le modèle physico-chimique comprenant les équations de Navier-Stokes et la cinétique chimique complexe est présenté dans la suite. Le troisième chapitre consiste en une étude comparative de différents schémas numériques de résolution des problèmes de type hyperbolique et présente une validation du code numérique développé autour du schéma TVD Upwind de Harten-Yee. Le traitement numérique des conditions aux limites et plus particulièrement des conditions de non-réflexion est présenté dans le chapitre suivant. Le reste de ce mémoire est consacré à l'interprétation de résultats de calculs de couches de mélange air-hydrogène (dans un premier temps inertes, puis réactives). Dans ce chapitre, une attention particulière a été portée sur l'étude phénoménologique du processus de mélange conditionné par les structures à grandes échelles. Par la suite les problèmes liés à l'interaction de ces structures avec onde de choc oblique sont abordés ; l'influence de ces structures sur le processus d'auto-allumage et sur la flamme qui en résulte est finalement analysée.
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Chakraborty, Debasis. "Confined Reacting Supersonic Mixing Layer - A DNS Study With Analysis Of Turbulence And Combustion Models." Thesis, 1998. http://etd.iisc.ernet.in/handle/2005/2167.

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Shivakanth, Chary P. "Linear Stability Models for Reacting Mixing Layers." Thesis, 2017. http://hdl.handle.net/2005/3267.

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We develop a physics-based reduced-order model of the aero-acoustic sound sources in reacting mixing layers as a method for fast and accurate predictions of the radiated sound. Instabilities in low-speed mixing layers are known to be dominated by the traditional Kelvin–Helmholtz (K–H)-type “central” mode, which is expected to be superseded by the “outer” modes as the chemical-reaction-based heat-release modifies the mean density, yielding new peaks in the density-weighted vorticity profiles. Although, these outer modes are known to be of lesser importance in the near-field mixing, how these radiate to the far-field is uncertain, on which we focus primarily, when the mixing layer is supersonic, but also report subsonic cases. On keeping the flow compressibility fixed, the outer modes are realized via biasing the respective mean density of the fast (oxidizer) or slow (fuel) side. In the linearized model that we use, the mean flow are laminar solutions of two-dimensional compressible boundary layers with an imposed composite turbulent spread rate, which we show to correctly predict the growth of instability waves by saturating them earlier, similar to in non-linear calculations, but obtained here via solving the linear parabolized stability equations (PSE). The chemical reaction is modeled via a single-step, single-product overall process which introduces a heat release term in the mean temperature equation. As the flow parameters are varied, modes that are unstable on the slow side are shown to be more sensitive to heat release, potentially exceeding equivalent central modes, as these modes yield relatively compact sound sources with lesser spreading of the mixing layer, when compared to the corresponding fast modes. In contrast, the radiated sound, obtained directly from the PSE solutions, seems to be relatively unaffected by a variation of mixture equivalence ratio, except for a lean mixture which is shown to yield a pronounced effect on the slow mode radiation by reducing its modal growth. For subsonic mixing layers, the sensitivity of central mode is explored, which in addition requires an acoustic analogy based method (e.g. the Lilley–Goldstein equations) to predict the sound from the linearized PSE sources, as used here, unlike in supersonic cases.
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Frieler, Clifford Eugene. "Mixing and reaction in the subsonic 2-D turbulent free shear layer." Thesis, 1992. https://thesis.library.caltech.edu/1197/1/Frieler_ce_1992.pdf.

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Several aspects of mixing and reaction in a turbulent two-dimensional shear layer have been studied. Experiments have been performed with reacting H2, F2, and NO in inert diluent gases. Sensing the heat release by these reactions, several aspects of the mixing process can be examined without the usual resolution limitations. For example, in contrast with direct measurements of composition, the amount of mixed fluid can be conservatively estimated with the results of the "flip" experiments. These have been performed over a range of density ratios, Reynolds numbers and heat release. The effects of initial conditions are of primary importance when comparisons to other studies are undertaken. Aspects as fundamental as growth rate of the turbulent region, or as obscure as the mixed fluid flux ratio depend strongly on the boundary conditions of this flow. These effects are examined in conjunction with those of Reynolds number and density ratio. For most cases studied here, tripping of the high speed boundary layer led to growth rate decreases. An exception was found for the case of high density ratio where the opposite effect was observed. This anomalous result occurred at conditions under which a new mode of instability has been shown to exist. Parallels exist between this unusual result and those of Batt in the uniform density case. An extensive study of the effects of density ratio on the mixing and reaction in the 2-D shear layer has been performed. Results indicate that several aspects of the mixing process are remarkably similar. Profiles of mixed fluid change little as the density ratio varies by a factor of 30. The integral amount of mixed fluid varies less than 6% for all density ratios examined. This insensitivity contrasts with that of the profiles of mixed fluid composition. While having very similar shapes the profiles are offset by an amount which depends very strongly upon the density ratio. The entrainment into the mixing layer has also been examined. Power spectral densities of the temperature time series were calculated and found to collapse upon normalization with the adiabatic flame temperature and large structure passage frequency. Least squares fits of the probability density functions were also examined. The initial work of Mungal and Frieler (1988) on the effects of chemical kinetics on the formation of product in the 2-D mixing layer have been greatly expanded. Measurements have been extended to include a wider range of NO concentrations and have been performed for two other stoichiometries. Results indicate that the simple model envisioned in Mungal and Frieler may only be suited for cases with extreme stoichiometry (very high or very low). Further investigations have turned up a serious discrepancy reflecting both on the experimental technique and on theory and modeling of this reacting flow. Experiments run under otherwise identical conditions demonstrate that more product is formed when F2 is the rich reactant than when H2 is the rich reactant. This dependence upon molecular character is counter intuitive and stems from a coupling of the effects of differing diffusivity and chemical kinetics. Numerical calculations based on simplified flow models are reported which demonstrate this coupling. These results indicate that even subtle diffusion effects can measurably effect reacting flows and imply that assumptions common among current modeling efforts must be re-examined. The effects of Reynolds number on mixing and reaction in the 2-D turbulent mixing layer have been examined. Evidence of the remnants of the initial roll up and mixing transition are seen for Reynolds numbers as large as 30,000. Indications of a resonance with the acoustic mode of the apparatus exist which affect results for Reynolds numbers up to 60,000. Natural transition of the high and low speed boundary layer on the splitter plate complicate comparisons of the high Reynolds number data with the remainder. In spite of all of these qualifications, the amount of mixed fluid is nearly constant. Over the range of Reynolds numbers 10,000 to 200,000, it varies by less than 12%. No evidence of an asymptotic decline in the amount of mixed fluid is observed.
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Books on the topic "Reacting Mixing Layer"

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United States. National Aeronautics and Space Administration., ed. A random distribution reacting mixing layer model. National Aeronautics and Space Administration, 1994.

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Drummond, J. Philip. A detailed numerical model of a supersonic reacting mixing layer. AIAA, 1986.

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Drummond, J. Philip. A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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Drummond, J. Philip. A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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Drummond, J. Philip. A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer. Langley Research Center, 1988.

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Drummond, J. Philip. A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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Drummond, J. Philip. A two-dimensional numerical simulation of a supersonic, chemically reacting mixing layer. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

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Jackson, Thomas L. Effect of heat release on the spatial stability of a supersonic reacting mixing layer. ICASE, 1988.

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Center, Lewis Research, ed. Mixing and non-equilibrium chemical reaction in a compressible mixing layer. State University of New York, 1991.

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Center, Lewis Research, ed. Mixing and non-equilibrium chemical reaction in a compressible mixing layer. State University of New York, 1991.

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Book chapters on the topic "Reacting Mixing Layer"

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Kessy, Edgard, Alexei Stoukov, and Dany Vandromme. "Numerical simulation of reacting mixing layer with a parallel implementation." In Lecture Notes in Computer Science. Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/3-540-60222-4_133.

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Pantano, Carlos, Sutanu Sarkar, and Forman Williams. "The Interaction of Scalar Mixing and Heat Release in a Reacting Shear Layer." In IUTAM Symposium on Turbulent Mixing and Combustion. Springer Netherlands, 2002. http://dx.doi.org/10.1007/978-94-017-1998-8_11.

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Lu, Di, and Fang Chen. "Effects of Tube Wall Thickness on Combustion and Growth Rate of Supersonic Reacting Mixing Layer." In Proceedings of the International Conference on Aerospace System Science and Engineering 2020. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-33-6060-0_16.

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Lee, C., R. W. Metcalfe, and F. Hussain. "Large Scale Structures in Reacting Mixing Layers." In Turbulent Shear Flows 7. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-76087-7_24.

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Grosch, C. E. "Reacting Compressible Mixing Layers: Structure and Stability." In ICASE/LaRC Interdisciplinary Series in Science and Engineering. Springer Netherlands, 1994. http://dx.doi.org/10.1007/978-94-011-1050-1_6.

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Miyauchi, Toshio, Mamoru Tanahashi, and Ye Li. "Sound Generation in Chemically Reacting Mixing Layers." In Smart Control of Turbulent Combustion. Springer Japan, 2001. http://dx.doi.org/10.1007/978-4-431-66985-2_3.

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Chollet, J. P., R. J. Gathmann, and M. R. Vallcorba. "Reactive Mixing Layers and Turbulent Combustion." In Advances in Turbulence 3. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-84399-0_30.

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Shin, Dongshin. "Instability of Wall-Bounded Compressible Reacting Mixing Layers." In Instability, Transition, and Turbulence. Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2956-8_39.

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Dimotakis, Paul E. "Turbulent Shear Layer Mixing With Fast Chemical Reactions." In Lecture Notes in Engineering. Springer US, 1989. http://dx.doi.org/10.1007/978-1-4613-9631-4_23.

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Ma, A. S. C., D. B. Spalding, and R. L. T. Sun. "Application of ESCIMO Theory to Turbulent Reacting Mixing Layers." In Recent Advances in the Aerospace Sciences. Springer US, 1985. http://dx.doi.org/10.1007/978-1-4684-4298-4_18.

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Conference papers on the topic "Reacting Mixing Layer"

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SHIN, D., and J. FERZIGER. "Stability of compressible reacting mixing layer." In 29th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-372.

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Jones, R., C. Marek, L. Myrabo, and H. Nagamatsu. "A random distribution reacting mixing layer model." In 30th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-3050.

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MILLER, M., T. ISLAND, J. SEITZMAN, C. BOWMAN, M. G. MUNGAL, and R. HANSON. "Compressibility effects in a reacting mixing layer." In 29th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1771.

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SHIN, D., and J. FERZIGER. "Linear stability of the reacting mixing layer." In 28th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-268.

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DRUMMOND, J., and M. HUSSAINI. "Numerical simulation of a supersonic reacting mixing layer." In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-1325.

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PLANCHE, O., and W. REYNOLDS. "Compressibility effects on the supersonic reacting mixing layer." In 29th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-739.

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Garrick, Sean. "Large Eddy Simulations of a turbulent reacting mixing layer." In 33rd Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-10.

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Chakraborty, Debasis, H. S. Mukunda, and P. J. Paul. "Effect of Stream Temperature on Hypervelocity Reacting Mixing Layer." In 41st Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-1205.

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Ferrero, Pietro, Anand Kartha, Pramod K. Subbareddy, Graham V. Candler, and Paul Dimotakis. "LES of a high-Reynolds number, chemically reacting mixing layer." In 43rd AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-3185.

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DRUMMOND, J., R. ROGERS, and M. HUSSAINI. "A detailed numerical model of a supersonic reacting mixing layer." In 22nd Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1427.

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Reports on the topic "Reacting Mixing Layer"

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Grosch, Chester. Reacting Compressible Mixing Layers: Structure and Stability. Defense Technical Information Center, 1993. http://dx.doi.org/10.21236/ada278319.

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Cetegen, B. M., and W. A. Sirignano. Analysis of Molecular Mixing and Chemical Reaction in Mixing Layer,. Defense Technical Information Center, 1988. http://dx.doi.org/10.21236/ada191600.

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