Auswahl der wissenschaftlichen Literatur zum Thema „Reactive premixted flow“
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Zeitschriftenartikel zum Thema "Reactive premixted flow"
Porumbel, Ionuţ, Andreea Cristina Petcu, Florin Gabriel Florean und Constantin Eusebiu Hritcu. „Artificial Neural Networks for Modeling of Chemical Source Terms in CFD Simulations of Turbulent Reactive Flows“. Applied Mechanics and Materials 555 (Juni 2014): 395–400. http://dx.doi.org/10.4028/www.scientific.net/amm.555.395.
Der volle Inhalt der QuelleKIM, SEUNG HYUN, und ROBERT W. BILGER. „Iso-surface mass flow density and its implications for turbulent mixing and combustion“. Journal of Fluid Mechanics 590 (15.10.2007): 381–409. http://dx.doi.org/10.1017/s0022112007008117.
Der volle Inhalt der QuelleMartin, S. M., J. C. Kramlich, G. Kosa´ly und J. J. Riley. „The Premixed Conditional Moment Closure Method Applied to Idealized Lean Premixed Gas Turbine Combustors“. Journal of Engineering for Gas Turbines and Power 125, Nr. 4 (01.10.2003): 895–900. http://dx.doi.org/10.1115/1.1587740.
Der volle Inhalt der QuelleWatanabe, Tomoaki, Yasuhiko Sakai, Kouji Nagata und Osamu Terashima. „Turbulent Schmidt number and eddy diffusivity change with a chemical reaction“. Journal of Fluid Mechanics 754 (30.07.2014): 98–121. http://dx.doi.org/10.1017/jfm.2014.387.
Der volle Inhalt der QuelleJames, S., M. S. Anand, M. K. Razdan und S. B. Pope. „In Situ Detailed Chemistry Calculations in Combustor Flow Analyses“. Journal of Engineering for Gas Turbines and Power 123, Nr. 4 (01.03.1999): 747–56. http://dx.doi.org/10.1115/1.1384878.
Der volle Inhalt der QuelleAlbayrak, Alp, Deniz A. Bezgin und Wolfgang Polifke. „Response of a swirl flame to inertial waves“. International Journal of Spray and Combustion Dynamics 10, Nr. 4 (20.12.2017): 277–86. http://dx.doi.org/10.1177/1756827717747201.
Der volle Inhalt der QuelleYang, Wenkai, Ashraf N. Al Khateeb und Dimitrios C. Kyritsis. „The Effect of Hydrogen Peroxide on NH3/O2 Counterflow Diffusion Flames“. Energies 15, Nr. 6 (17.03.2022): 2216. http://dx.doi.org/10.3390/en15062216.
Der volle Inhalt der QuelleSauer, Vinicius M., Fernando F. Fachini und Derek Dunn-Rankin. „Non-premixed swirl-type tubular flames burning liquid fuels“. Journal of Fluid Mechanics 846 (04.05.2018): 210–39. http://dx.doi.org/10.1017/jfm.2018.248.
Der volle Inhalt der QuelleZhang, Yun Peng, Xiang Yang Wei, Xing Huang und Bei Jing Zhong. „PAHs Formation Routes in the n-Heptane Laminar Flow Premixed Flame“. Applied Mechanics and Materials 361-363 (August 2013): 1062–66. http://dx.doi.org/10.4028/www.scientific.net/amm.361-363.1062.
Der volle Inhalt der QuelleLin, Ying, Xuesong Li, Martyn V. Twigg und William F. Northrop. „A non-premixed reactive volatilization reactor for catalytic partial oxidation of low volatility fuels at a short contact time“. Reaction Chemistry & Engineering 6, Nr. 4 (2021): 662–71. http://dx.doi.org/10.1039/d0re00460j.
Der volle Inhalt der QuelleDissertationen zum Thema "Reactive premixted flow"
Matino, Alessandra. „Characterisation of the Early Ignition Phase Generated by a Sunken Fire Igniter“. Electronic Thesis or Diss., Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique, 2024. http://www.theses.fr/2024ESMA0008.
Der volle Inhalt der QuelleEnvironmental restrictions tackle the reduction of the use of primary sources of energy motivating research to advance towards upgraded technologies. Alongside with these efforts, reliability and performance need to be ensured, especially for detrimental conditions of pressure and temperature, i.e. high altitude. In gas turbine engines, both these elements are crucial to offer products that fit to both the needs and expectations set by the present scenario. Ignition is a multiphase process constituted by several phases and events that span a diversified range of characteristic time scales. The numerical resolution of the early ignition phase, for which fine and detailed information is lacking, is investigated in this study. The efficiency of the igniter is estimated through calorimetry in pure air, which shows that variations of initial pressure have an influence on efficiency. The same investigation revealed that temperature (20° C; - 20°C) has a negligible effect. Physical properties of the kernel in terms of volume, surface, projection surface, radius of the arc channel in the cavity, are estimated adopting different optical diagnostics, including schlieren and shadowgraphy imaging at 1 MHz. Calculations are done to obtain a temporal evolution during energy depositing time (130 μs). An effect of initial pressure is observed on kernel properties such that reducing the initial pressure, kernel volume increases. Furthermore, filtered direct visualizations of the igniter cavity show that an effect of pressure is discerned from 20 μs. Kernel size is also measured for methane premixed mixtures of different equivalence ratios. This is intended to determine the influence of composition variation with respect to a reference case in pure N2 which is compared to measurements in gaseous premixed mixtures (both of inert CH4 / N2 and reactive CH4 / O2 / N2 nature). A comparison between inert and reactive cases exposes active combustion reactions already during energy deposition. To investigate the exposure to real life environment elements, the impact of a transverse flow at ambient conditions is studied in a wind tunnel. This was adapted to simulate the combined effect of a transverse flow and cooling air spilled from the liner that the igniter is exposed to by being mounted in a sleeve. The effect of the sleeve on kernel projection is investigated, which reveales an impact on projection and kernel deformation depending on the imposed velocity. The generation of the kernel is examined in a reactive premixed swirled mixture at 0.45 and 1 bar. The velocity field have been studied beforehand by PIV to know the velocity in the vicinity of the igniter and in the spatial domain where the kernel is projected. Three velocity conditions are retained to perform the discharge. Initial pressure is observed to influence the deformation the kernel undergoes depending on initial velocity. At 1 bar, the kernel appears to be preserved for longer. A secondary effect of equivalence ratio is found. The existing model of Taylor-Sedov is tested to predict kernel properties and compare them to experimental measurements. A preliminary study is performed to explore the interaction between the kernel and a spray at 0.45 bar and 1 bar. High magnification shadowgraphy is used to run statistics on a spatial window of 2 x 2 cm where droplets are observed impinging on the electrodes. Properties variations are detected depending on the synchronization with the discharge. Schlieren visualizations are further performed to observe phenomena to qualitatively explore the dynamics appearing in a time window of 1 ms
Smith, Thomas M. „Unsteady simulations of turbulent premixed reacting flows“. Diss., Georgia Institute of Technology, 1998. http://hdl.handle.net/1853/13097.
Der volle Inhalt der QuelleStevens, Eric John. „Velocity and scalar measurements in premixed turbulent reacting flows“. Thesis, University of Cambridge, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.624921.
Der volle Inhalt der QuelleAhrens, Denise [Verfasser]. „NOx-Formation in Reacting Premixed Jets in Hot Cross Flow / Denise Ahrens“. München : Verlag Dr. Hut, 2015. http://d-nb.info/1077404093/34.
Der volle Inhalt der QuelleYellugari, Kranthi. „Effects of Swirl Number and Central Rod on Flow in Lean Premixed Swirl Combustor“. University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1563872979440851.
Der volle Inhalt der QuelleWu, Men-Zan B. „Velocity and temperature measurements in a non-premixed reacting flow behind a backward facing step“. Diss., Georgia Institute of Technology, 1992. http://hdl.handle.net/1853/12045.
Der volle Inhalt der QuelleIto, Yasumasa. „Promotion of fluid mixing and chemical reaction in non-premixed liquid flows“. 京都大学 (Kyoto University), 2007. http://hdl.handle.net/2433/136342.
Der volle Inhalt der QuellePaul, Sreebash Chandra. „Large eddy simulation of a fuel-rich turbulent non-premixed reacting flow with radiative heat transfer“. Thesis, University of Glasgow, 2008. http://theses.gla.ac.uk/203/.
Der volle Inhalt der QuelleTokekar, Devkinandan Madhukar. „Modeling and simulation of reacting flows in lean-premixed swirl-stabilized gas turbine combustor“. Cincinnati, Ohio : University of Cincinnati, 2005. http://www.ohiolink.edu/etd/view.cgi?acc%5Fnum=ucin1141412599.
Der volle Inhalt der QuelleTitle from electronic thesis title page (viewed Apr. 18, 2006). Includes abstract. Keywords: Large Eddy Simulation; LES; Lean Pre-mixed; LPM; Gas Turbine Combustor; Combustion; Reacting Flows. Includes bibliographical references.
TOKEKAR, DEVKINANDAN MADHUKAR. „MODELING AND SIMULATION OF REACTING FLOWS IN LEAN-PREMIXED SWIRL-STABLIZED GAS TURBINE COMBUSTOR“. University of Cincinnati / OhioLINK, 2006. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1141412599.
Der volle Inhalt der QuelleBücher zum Thema "Reactive premixted flow"
C, So Ronald M., und United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Hrsg. On the modelling of non-reactive and reactive turbulent combustor flows. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Den vollen Inhalt der Quelle findenNikjooy, Mohammad. On the modelling of non-reactive and reactive turbulent combustor flows. Cleveland, Ohio: Lewis Research Center, 1987.
Den vollen Inhalt der Quelle findenWu, Men-Zan Bill. Velocity and temperature measurements in a non-premixed reacting flow behind a backward facing step. Atlanta, Ga: Georgia Institute of Technology, 1992.
Den vollen Inhalt der Quelle findenOn the modelling of non-reactive and reactive turbulent combustor flows. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Den vollen Inhalt der Quelle findenBuchteile zum Thema "Reactive premixted flow"
Iavarone, S., H. Yang, Z. Li, Z. X. Chen und N. Swaminathan. „On the Use of Machine Learning for Subgrid Scale Filtered Density Function Modelling in Large Eddy Simulations of Combustion Systems“. In Lecture Notes in Energy, 209–43. Cham: Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-16248-0_8.
Der volle Inhalt der QuelleHamel, F., und R. Monneau. „Conical-Shaped Travelling Fronts Allied to the Mathematical Analysis of the Shape of Premixed Bunsen Flames“. In Nonlinear PDE’s in Condensed Matter and Reactive Flows, 169–87. Dordrecht: Springer Netherlands, 2002. http://dx.doi.org/10.1007/978-94-010-0307-0_8.
Der volle Inhalt der Quelle„Flows with Premixed Reactants“. In An Introduction to Turbulent Reacting Flows, 87–132. PUBLISHED BY IMPERIAL COLLEGE PRESS AND DISTRIBUTED BY WORLD SCIENTIFIC PUBLISHING CO., 2007. http://dx.doi.org/10.1142/9781848161368_0005.
Der volle Inhalt der Quelle„Flows with Non-premixed Reactants“. In An Introduction to Turbulent Reacting Flows, 63–86. PUBLISHED BY IMPERIAL COLLEGE PRESS AND DISTRIBUTED BY WORLD SCIENTIFIC PUBLISHING CO., 2007. http://dx.doi.org/10.1142/9781848161368_0004.
Der volle Inhalt der Quelle„Extinction of Premixed Curved Flames Stabilized in a Stagnation Flow“. In Dynamics of Deflagrations and Reactive Systems: Flames, 161–75. Washington DC: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/5.9781600866043.0161.0175.
Der volle Inhalt der Quelle„Laminar Premixed Flames: Simulation of Combustion in the Flame Front“. In Chemical Kinetics in Combustion and Reactive Flows, 207–27. Cambridge University Press, 2019. http://dx.doi.org/10.1017/9781108581714.004.
Der volle Inhalt der Quelle„Flame Curvature and Flame Speed of a Turbulent Premixed Flame in a Stagnation Point Flow“. In Dynamics of Heterogeneous Combustion and Reacting Systems, 25–36. Washington DC: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/5.9781600866258.0025.0036.
Der volle Inhalt der QuelleKoutmos, P., C. Mavridis und D. Papailiou. „A study of turbulent isothermal and non-premixed reacting wake flows past a two-dimensional square cylinder.“ In Engineering Turbulence Modelling and Experiments, 797–806. Elsevier, 1996. http://dx.doi.org/10.1016/b978-0-444-82463-9.50082-4.
Der volle Inhalt der QuelleKonferenzberichte zum Thema "Reactive premixted flow"
Wahid, Mazlan A., M. Z. Ahmad Faiz, M. A. Wahid, S. Samion, N. A. C. Sidik und J. M. Sheriff. „Swirling Lean-Premixed Reacting Flow“. In THE 10TH ASIAN INTERNATIONAL CONFERENCE ON FLUID MACHINERY. AIP, 2010. http://dx.doi.org/10.1063/1.3464844.
Der volle Inhalt der QuelleKru¨ger, Oliver, Katharina Go¨ckeler, Sebastian Go¨ke, Christian Oliver Paschereit, Christophe Duwig und Laszlo Fuchs. „Numerical Investigations of a Swirl-Stabilized Premixed Flame at Ultra-Wet Conditions“. In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-45866.
Der volle Inhalt der QuelleHamlington, Peter, Alexei Poludnenko und Elaine Oran. „Intermittency and Premixed Turbulent Reacting Flows“. In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-113.
Der volle Inhalt der QuelleMartin, Scott M., John C. Kramlich, George Kosa´ly und James J. Riley. „The Premixed Conditional Moment Closure Method Applied to Idealized Lean Premixed Gas Turbine Combustors“. In ASME Turbo Expo 2002: Power for Land, Sea, and Air. ASMEDC, 2002. http://dx.doi.org/10.1115/gt2002-30094.
Der volle Inhalt der QuelleSantosh Kumar, T. V., P. R. Alemela und J. B. W. Kok. „Dynamics of Flame Stabilized by Triangular Bluff Body in Partially Premixed Methane-Air Combustion“. In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-46241.
Der volle Inhalt der QuelleMulas, Marco, und Marco Talice. „Fully Compressible Simulation of Low-Speed Premixed Reactive Flows“. In 33rd AIAA Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-4253.
Der volle Inhalt der QuelleDe, Ashoke, Shengrong Zhu und Sumanta Acharya. „An Experimental and Computational Study of a Swirl-Stabilized Premixed Flame“. In ASME Turbo Expo 2009: Power for Land, Sea, and Air. ASMEDC, 2009. http://dx.doi.org/10.1115/gt2009-60230.
Der volle Inhalt der QuelleJames, S., M. S. Anand, M. K. Razdan und S. B. Pope. „In Situ Detailed Chemistry Calculations in Combustor Flow Analyses“. In ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/99-gt-271.
Der volle Inhalt der QuelleUchiyama, Tomomi, und Naohiro Otsuki. „Numerical Simulation for Free Turbulent Reacting Flow by Particle Method“. In ASME/JSME 2003 4th Joint Fluids Summer Engineering Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/fedsm2003-45289.
Der volle Inhalt der QuelleChakravorty, Saugata, und Joseph Mathew. „Explicit Filtering LES for Turbulent Non-Premixed Combustion“. In ASME/JSME 2007 5th Joint Fluids Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/fedsm2007-37361.
Der volle Inhalt der QuelleBerichte der Organisationen zum Thema "Reactive premixted flow"
Chapman und Toema. PR-266-07209-R01 Phase 2 - Assessment of the Robustness and Transportability of the Gas Turbine Model. Chantilly, Virginia: Pipeline Research Council International, Inc. (PRCI), Dezember 2010. http://dx.doi.org/10.55274/r0010719.
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