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Relevant bibliographies by topics / Two phase flow combustion

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Academic literature on the topic 'Two phase flow combustion'

Author: Grafiati

Published: 7 July 2024

Last updated: 31 July 2025

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Journal articles on the topic "Two phase flow combustion"

1

Tolpadi, A. K. "Calculation of Two-Phase Flow in Gas Turbine Combustors." Journal of Engineering for Gas Turbines and Power 117, no. 4 (1995): 695–703. http://dx.doi.org/10.1115/1.2815455.

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A method is presented for computing steady two-phase turbulent combusting flow in a gas turbine combustor. The gas phase equations are solved in an Eulerian frame of reference. The two-phase calculations are performed by using a liquid droplet spray combustion model and treating the motion of the evaporating fuel droplets in a Lagrangian frame of reference. The numerical algorithm employs nonorthogonal curvilinear coordinates, a multigrid iterative solution procedure, the standard k-ε turbulence model, and a combustion model comprising an assumed shape probability density function and the cons

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2

Klose, G., R. Schmehl, R. Meier, et al. "Evaluation of Advanced Two-Phase Flow and Combustion Models for Predicting Low Emission Combustors." Journal of Engineering for Gas Turbines and Power 123, no. 4 (2000): 817–23. http://dx.doi.org/10.1115/1.1377010.

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The development of low-emission aero-engine combustors strongly depends on the availability of accurate and efficient numerical models. The prediction of the interaction between two-phase flow and chemical combustion is one of the major objectives of the simulation of combustor flows. In this paper, predictions of a swirl stabilized model combustor are compared to experimental data. The computational method is based on an Eulerian two-phase model in conjunction with an eddy dissipation (ED) and a presumed-shape-PDF (JPDF) combustion model. The combination of an Eulerian two-phase model with a

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3

Som, S. K., and N. Y. Sharma. "Energy and Exergy Balance in the Process of Spray Combustion in a Gas Turbine Combustor." Journal of Heat Transfer 124, no. 5 (2002): 828–36. http://dx.doi.org/10.1115/1.1484393.

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A theoretical model of exergy balance based on availability transfer and flow availability in the process of spray combustion in a gas turbine combustor has been developed to evaluate the total thermodynamic irreversibility and second law efficiency of the process at various operating conditions, for fuels with different volatilities. The velocity, temperature and concentration fields in the combustor, required for the evaluation of the flow availabilities and process irreversibilities, have been computed numerically from a two phase separated flow model of spray combustion. The total thermody

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Zhang, Qun, Hua Sheng Xu, Tao Gui, Shun Li Sun, Yue Wu, and Dong Bo Yan. "Investigation on Reaction Flow Field of Low Emission TAPS Combustors." Applied Mechanics and Materials 694 (November 2014): 45–48. http://dx.doi.org/10.4028/www.scientific.net/amm.694.45.

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A twin annular premixing swirler (TAPS) combustor model of low emissions was developed in this study. And computational studies on combustion process in the combustor model were carried out. Standard k-ε Turbulence Model, PDF non-premixed combustion model, Zeldovich thermal NOx formation model and DPM two-phase model were employed. The distributions of some key performance parameters such as gas temperature, flow velocity, concentrations of NOx and CO emissions were obtained and analyzed. At the same time, combustion mechanics inside the TAPS combustor model were investigated. The computationa

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5

Lin, Jih Lung. "Two-phase flow effect on hybrid rocket combustion." Acta Astronautica 65, no. 7-8 (2009): 1042–57. http://dx.doi.org/10.1016/j.actaastro.2009.03.020.

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Som, S. K., S. S. Mondal, and S. K. Dash. "Energy and Exergy Balance in the Process of Pulverized Coal Combustion in a Tubular Combustor." Journal of Heat Transfer 127, no. 12 (2005): 1322–33. http://dx.doi.org/10.1115/1.2101860.

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A theoretical model of exergy balance, based on availability transfer and flow availability, in the process of pulverized coal combustion in a tubular air-coal combustor has been developed to evaluate the total thermodynamic irreversibility and second law efficiency of the process at various operating conditions. The velocity, temperature, and concentration fields required for the evaluation of flow availability have been computed numerically from a two-phase separated flow model on a Eulerian-Lagrangian frame in the process of combustion of pulverized coal particles in air. The total thermody

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Chan, S. H., and M. M. M. Abou-Ellail. "A Two-Fluid Model for Reacting Turbulent Two-Phase Flows." Journal of Heat Transfer 116, no. 2 (1994): 427–35. http://dx.doi.org/10.1115/1.2911415.

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A reacting two-fluid model, based on the solution of separate transport equations for reacting gas-liquid two-phase flow, is presented. New time-mean transport equations for two-phase mixture fraction f and its variance g are derived. The new two-fluid transport equations for f and g are useful for two-phase reacting flows in which phases strongly interact. They are applicable to both submerged and nonsubmerged combustion. A pdf approach to the reaction process is adopted. The mixture fraction pdf assumes the shape of a beta function while the instantaneous thermochemical properties are comput

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Zhang, Xiang Yu, Guo Qiang He, Pei Jin Liu, and Jiang Li. "Heat Flux Measurement Method of Two-Phase Flow in SRM." Applied Mechanics and Materials 152-154 (January 2012): 883–88. http://dx.doi.org/10.4028/www.scientific.net/amm.152-154.883.

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Accurate information on heat transfer data of combustion products in the solid rocket motor chamber is a crucial prerequisite for the engine thermal protection. A measurement technique was well developed to acquire steady-state heat flux data of two-phase flow and was used successfully in the hostile environment. Experimental heat flux measurement has been obtained with an innovative designed instrument by simulating the flow field of complex charging configuration. The total heat flux of combustion products in the chamber was brought away by the coolant and calculated by its enthalpy rise in

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Ahmad Fuad Abdul Rasid and Yang Zhang. "Combustion Phases of Evaporating Neat Fuel Droplet." Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 96, no. 1 (2022): 60–69. http://dx.doi.org/10.37934/arfmts.96.1.6069.

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The combustion characteristics of fuel spray can be examined at a basic level by a fuel droplet combustion study. Evaporation processes of a fuel droplet involves few combustion phases mainly heating, boiling and disruptive phase. The transition of phases is found to be caused by two transient combustion process; mainly droplet heating and fuel vapour accumulation. The duration of combustion phases of tested neat fuel droplet in the present work is found to be consistent for each fuel. High volatility fuel is found to have the shortest duration of droplet heating and fuel vapour accumulation.

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Hsiao Tzu, Chang, Hourng Lih Wu, and Lai Chen Chien. "Nonequilibrium hydrogen combustion in one- and two-phase supersonic flow." International Communications in Heat and Mass Transfer 24, no. 3 (1997): 323–35. http://dx.doi.org/10.1016/s0735-1933(97)00018-3.

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Dissertations / Theses on the topic "Two phase flow combustion"

1

Carabateas, Nicolas. "Two phase flow and combustion in S.I. engines." Thesis, Imperial College London, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.265853.

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Sankaran, Vaidyanathan. "Sub-grid Combustion Modeling for Compressible Two-Phase Flows." Diss., Georgia Institute of Technology, 2003. http://hdl.handle.net/1853/5274.

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A generic formulation for modeling the sub-grid combustion in compressible, high Reynolds number, two-phase, reacting flows has been developed and validated. A sub-grid mixing/combustion model called Linear Eddy Mixing (LEM) model has been extended to compressible flows and used inside the framework of Large Eddy Simulation (LES) in this LES-LEM approach. The LES-LEM approach is based on the proposition that the basic mechanistic distinction between the convective and the molecular effects should be preserved for accurate prediction of the complex flow-fields such as those encountered in many

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Rochette, Bastien. "Modeling and simulation of two-phase flow turbulent combustion in aeronautical engines." Thesis, Toulouse, INPT, 2019. http://www.theses.fr/2019INPT0059.

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De nos jours, plus de 80% de l'énergie consommée sur Terre provient de la combustion de combustibles fossiles. Des solutions alternatives à la combustion sont en cours de développement mais les contraintes spécifiques liées au transport aérien ne permettent pas actuellement d'alimenter des moteurs sans introduire de rupture technologique. Ces résultats expliquent les activités de recherche visant à améliorer les connaissances et le contrôle des processus de combustion afin de concevoir des moteurs aéronautiques plus propres et plus efficaces. Dans ce cadre, les Simulations aux Grandes Echelles

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Collin, Félix. "Modeling and numerical simulations of two-phase ignition in gas turbine." Thesis, Toulouse, INPT, 2019. http://www.theses.fr/2019INPT0053.

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Afin de répondre aux nouvelles réglementations environnementales internationales tout en maintenant une forte compétitivité économique, des technologies innovantes de chambres de combustion aéronautiques sont développées. Ces technologies doivent garantir un rallumage rapide en cas d’extinction, qui est un des aspects les plus critiques et complexes de la conception moteur. La maîtrise de cette phase implique une compréhension approfondie des phénomènes physiques mis en jeu. Dans cette thèse la séquence d’allumage diphasique de moteur aéronautique a été étudiée dans son intégralité, du claquag

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Thawley, Scott. "Spatio-temporal Characteristics of a Spray from a Liquid Jet in Crossflow." Thesis, Virginia Tech, 2006. http://hdl.handle.net/10919/31276.

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A liquid jet in a crossflow is often used to as a fuel injection method for combustion systems. Parameters such as penetration and core trajectory are used as characterization for the spray and specification of design criteria for combustor geometry. In addition to penetration and core trajectory, mapping the mass flux in space and time is an important part of modeling evaporation and global equivalence ratio throughout the combustor. Accurate prediction of these spray characteristics allows for a stable and robust combustor design. The break up of a liquid jet in a crossflow is an extremel

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Caceres, Marcos. "Impact of transverse acoustic modes on a linearly arranged two-phase flow swirling flames." Thesis, Normandie, 2019. http://www.theses.fr/2019NORMIR01/document.

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Les besoins énergétiques de la population mondiale ne cessent d’augmenter. Les prévisions indiquent par exemple une forte croissance de la demande du secteur du transport aéronautique. La recherche de systèmes toujours plus performants et moins polluants est nécessaire. Des nouveaux concepts pour la combustion ont été mis au point et appliqués aux turbines à gaz. Parmi eux il existe ceux basés sur la combustion en prémélange pauvre ou en prémélange pauvre pré-vaporisé dans le cas où le carburant utilisé est liquide. Les nouveaux systèmes énergétiques basés sur la combustion en régime pauvre so

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Eyssartier, Alexandre. "LES of two-phase reacting flows : stationary and transient operating conditions." Thesis, Toulouse, INPT, 2012. http://www.theses.fr/2012INPT0011/document.

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L'allumage et le réallumage de haute altitude présentent de grandes difficultés dans le cadre des chambres de combustion aéronautiques. Le succès d'un allumage dépend de multiples facteurs, des caractéristiques de l'allumeur à la taille des gouttes du spray en passant par le niveau de turbulence au point d'allumage. Déterminer la position optimale de l'allumeur ou le potentiel d'allumage d'une source d'énergie donnée à une position donnée sont ainsi des paramètres essentiels lors du design de chambre de combustion. Le but de ces travaux de thèse est d'étudier l'allumage forcé des chambres de c

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Nelson, Lauren May. "Rayleigh Flow of Two-Phase Nitrous Oxide as a Hybrid Rocket Nozzle Coolant." DigitalCommons@CalPoly, 2009. https://digitalcommons.calpoly.edu/theses/284.

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The Mechanical Engineering Department at California Polytechnic State University in San Luis Obispo currently maintains a lab-scale hybrid rocket motor for which nitrous oxide is utilized as the oxidizer in the combustion system. Because of its availability, the same two-phase (gas and liquid) nitrous oxide that is used in the combustion system is also routed around the throat of the hybrid rocket’s converging-diverging nozzle as a coolant. While this coolant system has proven effective empirically in previous tests, the physics behind the flow of the two-phase mixture is largely unexplained.

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Akritopoulos, Michail. "Combustion modelling of dispersed two-phase flows, applied in circulating fluidised beds." Thesis, Imperial College London, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.414215.

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Overbrüggen, Timo van [Verfasser], Wolfgang [Akademischer Betreuer] Schröder, and Reinhold [Akademischer Betreuer] Kneer. "Experimental analysis of the two-phase flow field in internal combustion engines / Timo van Overbrüggen ; Wolfgang Schröder, Reinhold Kneer." Aachen : Universitätsbibliothek der RWTH Aachen, 2016. http://d-nb.info/1125911573/34.

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Books on the topic "Two phase flow combustion"

1

Nguyen, Hung Lee. Two-dimensional analysis of two-phase reacting flow in a firing direct-injection diesel engine. National Aeronautics and Space Administration, Lewis Research Center, 1989.

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Center, Lewis Research, ed. Two-dimensional analysis of two-phase reacting flow in a firing direct-injection diesel engine. National Aeronautics and Space Administration, Lewis Research Center, 1989.

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Center, Lewis Research, ed. Two-dimensional analysis of two-phase reacting flow in a firing direct-injection diesel engine. National Aeronautics and Space Administration, Lewis Research Center, 1989.

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4

I͡Arin, Leonid Petrovich. Osnovy teorii gorenii͡a dvukhfaznykh sred. Ėnergoatomizdat, Leningradskoe otd-nie, 1987.

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Center, Lewis Research, ed. LSPRAY: A Lagrangian spray solver, user's manual : prepared under contract NAS3-27186. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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6

C, Roco M., ed. Particulate two-phase flow. Butterworth-Heinemann, 1993.

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7

Yarin, L. P., and G. Hetsroni. Combustion of Two-Phase Reactive Media. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-06299-9.

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Yarin, L. P. Combustion of Two-Phase Reactive Media. Springer Berlin Heidelberg, 2004.

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9

Gad, Hetsroni, ed. Combustion of two-phase reactive media. Springer, 2004.

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10

Kakaç, Sadik, Arthur E. Bergles, and E. Oliveira Fernandes, eds. Two-Phase Flow Heat Exchangers. Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2790-2.

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Book chapters on the topic "Two phase flow combustion"

1

Poinsot, Thierry. "Two-Phase Flow Combustion." In Instabilities of Flows: With and Without Heat Transfer and Chemical Reaction. Springer Vienna, 2010. http://dx.doi.org/10.1007/978-3-7091-0127-8_10.

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2

Coward, Adrian V., and Philip Hall. "On the Instability of Two-Phase Stagnation Point Flow." In Transition, Turbulence and Combustion. Springer Netherlands, 1994. http://dx.doi.org/10.1007/978-94-011-1032-7_16.

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3

Durst, F., and T. Börner. "Dispersed Two-Phase Flows, its Experimental Investigation and Numerical Prediction." In Instrumentation for Combustion and Flow in Engines. Springer Netherlands, 1989. http://dx.doi.org/10.1007/978-94-009-2241-9_17.

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Tai, Lv, and Ting-ting Zhou. "Numerical Simulation of Two Phase Flow Characteristic in Dynamic-Static Separator." In Cleaner Combustion and Sustainable World. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-30445-3_137.

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Dimitrova, D., M. Braun, J. Janicka, and A. Sadiki. "Large Eddy Simulation of Dispersed Two-Phase Flows and Premixed Combustion in IC-Engines." In Flow and Combustion in Advanced Gas Turbine Combustors. Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5320-4_14.

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Diakoumakos, E., J. Anagnostopoulos, and G. Bergeles. "A Theoretical Study of Air-Solid Two-Phase Flows." In Mathematical Modeling in Combustion and Related Topics. Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2770-4_30.

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Marchesin, Dan, Jesus da Mota, and Aparecido de Souza. "Riemann Solutions for a Model of Combustion in Two-Phase Flow in Porous Media." In Hyperbolic Problems: Theory, Numerics, Applications. Birkhäuser Basel, 2001. http://dx.doi.org/10.1007/978-3-0348-8372-6_22.

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de Vicente, S., G. Galiano, J. Velasco, and J. M. Aróstegui. "Mathematical Description of the Hydrodynamic Regimes of an Asymptotic Model for Two-Phase Flow Arising in PFBC Boilers." In Proceedings of the 20th International Conference on Fluidized Bed Combustion. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-02682-9_135.

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Nguyen, Van Bo, Li Jiun-Ming, Teo Chiang Juay, and Boo-Cheong Khoo. "Numerical Simulation of Combustion Process for Two-Phase Fuel Flows Related to Pulse Detonation Engines." In 30th International Symposium on Shock Waves 1. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-46213-4_67.

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Bourgeat, Alain. "Two-Phase Flow." In Interdisciplinary Applied Mathematics. Springer New York, 1997. http://dx.doi.org/10.1007/978-1-4612-1920-0_5.

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Conference papers on the topic "Two phase flow combustion"

1

Hebrard, P., J. Courquet, and G. Lavergne. "Numerical Simulation of Two-Phase Flow in Combustion Chambers." In ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1991. http://dx.doi.org/10.1115/91-gt-112.

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The purpose of this paper is to describe a new approach in which one uses different kinds of post processing to obtain, from 2D or 3D computation codes, the representation of internal flow inside a combustion chamber as an association of elementary reactors (well stirred, plug flow…) To reach this goal and, in order to test this method, different computation codes are used for the gas phase description: mean flow computation or unsteady codes like “R.V.M.” (Random Vortex Method) or “F.C.T.” (Flux corrected transport) - For the liquid phase behaviour, we use to kinds of Lagrangian transport sch

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2

Stowe, R., C. Dubois, P. Harris, A. Mayer, A. De Champlain, and S. Ringuette. "Two phase flow combustion modelling of a ducted rocket." In 37th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3461.

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Mittal, M., and T. Rozmajzl. "Numerical simulation of two-phase fluid flow for combustion." In 34th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-708.

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Klose, G., R. Schmehl, R. Meier, et al. "Evaluation of Advanced Two-Phase Flow and Combustion Models for Predicting Low Emission Combustors." In ASME Turbo Expo 2000: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/2000-gt-0133.

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The development of low emission aero engine combustors strongly depends on the availability of accurate and efficient numerical models. The prediction of the interaction between two-phase flow and chemical combustion is one of the major objectives of the simulation of combustor flows. In this paper, predictions of a swirl stabilized model combustor are compared to experimental data. The computational method is based on an Eulerian two-phase model in conjunction with an Eddy Dissipation (ED) and a presumed-shape-PDF (JPDF) combustion model. The combination of an Eulerian two-phase model with a

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Saha, Kaushik, and Xianguo Li. "Assessment of Different Cavitation Models in Mixture and Eulerian Framework for Two-Phase Flow in Diesel Injectors." In ASME 2013 Internal Combustion Engine Division Fall Technical Conference. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/icef2013-19201.

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A comparative study using different cavitation models in mixture and Eulerian framework is carried out for the analysis of two-phase flows in diesel injectors. Three different cavitation models are investigated here: recently developed modified single-fluid, Schnerr-Sauer and Zwart-Gerber-Belamri models. The last two models have been implemented in both mixture and Eulerian framework. The numerical predictions are compared both qualitatively and quantitatively with experimental results available in the literature. Qualitative assessments have been carried out with experimental images of two-ph

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Li, Zhaorui, Murat Yaldizli, and Farhad A. Jaberi. "Numerical Simulations of Two-Phase Turbulent Combustion in Spray Burners." In ASME 2007 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/detc2007-35433.

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The complex interactions among turbulence, combustion and spray in liquid-fuel burners are modeled and simulated via a new two-phase Lagrangian-Eulerian-Lagrangian large eddy simulation (LES) methodology. In this methodology, the spray is modeled with a Lagrangian mathematical/computational method which allows two-way mass, momentum and energy coupling between phases. The subgrid gas-liquid combustion is based on the two-phase filtered mass density function (FMDF) that has several advantages over “conventional” two-phase combustion models. The LES/FMDF is employed in conjunction with non-equil

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von Langenthal, Thomas, Nikolaos Zarzalis, and Alexandra Loukou. "Experimental Two-Phase Flow Analysis Inside a Laboratory Scale Jet-Engine Combustion Chamber Using PIV." In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-14476.

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Abstract The characterization of the two-phase kerosene/air flow near the nozzle of an aero engine combustor is important in order to understand the combustion characteristics of the burner. Typically, Particle Image Velocimetry (PIV) or Laser Doppler Velocimetry (LDV) is used to measure velocities inside aero engine combustors. However, these measurement techniques rely on tracer particles to visualize the flow field and are usually only able to measure the velocity field of one phase at a time. In the case of PIV measurements both the flow tracers and the kerosene droplets scatter the laser

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YU, F. "Hydraulic analogy application in the study of a two-phase mixture combustion flow." In 28th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-451.

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Dong, Ming, Maozhao Xie, and Hong Liu. "Numerical Study on Turbulent Two-Phase Flow in a Porous Media Combustion Chamber." In 2008 SAE International Powertrains, Fuels and Lubricants Congress. SAE International, 2008. http://dx.doi.org/10.4271/2008-01-1592.

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Srinivasan, Navneeth, Hongyuan Zhang, and Suo Yang. "A VLE-Based Reacting Flow Solver for High-Pressure Transcritical Two-Phase Combustion." In AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-1858.

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Reports on the topic "Two phase flow combustion"

1

Luke, Gary, Mark Eagar, Michael Sears, Scott Felt, and Bob Prozan. Status of Advanced Two-Phase Flow Model Development for SRM Chamber Flow Field and Combustion Modeling. Defense Technical Information Center, 2004. http://dx.doi.org/10.21236/ada427829.

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Cizmas, Paul, and Antonio Palacios. A REDUCED ORDER MODEL OF TWO-PHASE FLOW, HEAT TRANSFER AND COMBUSTION IN CIRCULATING FLUIDIZED-BEDS. Office of Scientific and Technical Information (OSTI), 2001. http://dx.doi.org/10.2172/792073.

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Paul Cizmas. A REDUCED ORDER MODEL OF TWO-PHASE FLOW, HEAT TRANSFER AND COMBUSTION IN CIRCULATING FLUIDIZED-BEDS. Office of Scientific and Technical Information (OSTI), 2003. http://dx.doi.org/10.2172/827038.

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Paul Cizmas. A REDUCED ORDER MODEL OF TWO-PHASE FLOW, HEAT TRANSFER AND COMBUSTION IN CIRCULATING FLUIDIZED-BEDS. Office of Scientific and Technical Information (OSTI), 2002. http://dx.doi.org/10.2172/813624.

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Chapman and Toema. PR-266-07209-R01 Phase 2 - Assessment of the Robustness and Transportability of the Gas Turbine Model. Pipeline Research Council International, Inc. (PRCI), 2010. http://dx.doi.org/10.55274/r0010719.

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This report presents the modeling study of a gas turbine combustor based on first engineering principles to fully characterize the nitrogen oxides (NOx) and carbon monoxide emissions (CO). The model is mainly focused on the emissions from the widely used lean-premixed, dry low-NOx combustor. The combustor is divided into several zones where each zone can be considered as a plug-flow reactor. Each of these zones is assumed to have a uniform pressure, temperature and perfect mixing between combustion species. The temperature of each zone is calculated using mass and energy balances along with he

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Wallis, G. B. Two phase potential flow. Office of Scientific and Technical Information (OSTI), 1991. http://dx.doi.org/10.2172/6213215.

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Maeder, P. F., and J. Kestin. Two-phase flow in geothermal systems. Office of Scientific and Technical Information (OSTI), 1987. http://dx.doi.org/10.2172/5984665.

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Farwagi, S. M. Computer Modelling of Two-Phase Flow. Defense Technical Information Center, 1986. http://dx.doi.org/10.21236/ada175048.

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Wallis, G. B. Two-Phase Potential Flow. Final report. Office of Scientific and Technical Information (OSTI), 1999. http://dx.doi.org/10.2172/761114.

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Theilacker, Jay, and C. Rode. An Investigation Into Flow Regimes for Two Phase Helium Flow. Office of Scientific and Technical Information (OSTI), 1987. http://dx.doi.org/10.2172/1151469.

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