Auswahl der wissenschaftlichen Literatur zum Thema „Two phase flow combustion“
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Zeitschriftenartikel zum Thema "Two phase flow combustion"
Tolpadi, A. K. „Calculation of Two-Phase Flow in Gas Turbine Combustors“. Journal of Engineering for Gas Turbines and Power 117, Nr. 4 (01.10.1995): 695–703. http://dx.doi.org/10.1115/1.2815455.
Der volle Inhalt der QuelleKlose, G., R. Schmehl, R. Meier, G. Maier, R. Koch, S. Wittig, M. Hettel, W. Leuckel und N. Zarzalis. „Evaluation of Advanced Two-Phase Flow and Combustion Models for Predicting Low Emission Combustors“. Journal of Engineering for Gas Turbines and Power 123, Nr. 4 (01.10.2000): 817–23. http://dx.doi.org/10.1115/1.1377010.
Der volle Inhalt der QuelleSom, S. K., und N. Y. Sharma. „Energy and Exergy Balance in the Process of Spray Combustion in a Gas Turbine Combustor“. Journal of Heat Transfer 124, Nr. 5 (11.09.2002): 828–36. http://dx.doi.org/10.1115/1.1484393.
Der volle Inhalt der QuelleLin, Jih Lung. „Two-phase flow effect on hybrid rocket combustion“. Acta Astronautica 65, Nr. 7-8 (Oktober 2009): 1042–57. http://dx.doi.org/10.1016/j.actaastro.2009.03.020.
Der volle Inhalt der QuelleZhang, Qun, Hua Sheng Xu, Tao Gui, Shun Li Sun, Yue Wu und 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.
Der volle Inhalt der QuelleChan, S. H., und M. M. M. Abou-Ellail. „A Two-Fluid Model for Reacting Turbulent Two-Phase Flows“. Journal of Heat Transfer 116, Nr. 2 (01.05.1994): 427–35. http://dx.doi.org/10.1115/1.2911415.
Der volle Inhalt der QuelleSom, S. K., S. S. Mondal und S. K. Dash. „Energy and Exergy Balance in the Process of Pulverized Coal Combustion in a Tubular Combustor“. Journal of Heat Transfer 127, Nr. 12 (25.07.2005): 1322–33. http://dx.doi.org/10.1115/1.2101860.
Der volle Inhalt der QuelleZhang, Xiang Yu, Guo Qiang He, Pei Jin Liu und Jiang Li. „Heat Flux Measurement Method of Two-Phase Flow in SRM“. Applied Mechanics and Materials 152-154 (Januar 2012): 883–88. http://dx.doi.org/10.4028/www.scientific.net/amm.152-154.883.
Der volle Inhalt der QuelleHsiao Tzu, Chang, Hourng Lih Wu und Lai Chen Chien. „Nonequilibrium hydrogen combustion in one- and two-phase supersonic flow“. International Communications in Heat and Mass Transfer 24, Nr. 3 (Mai 1997): 323–35. http://dx.doi.org/10.1016/s0735-1933(97)00018-3.
Der volle Inhalt der QuelleAhmad Fuad Abdul Rasid und Yang Zhang. „Combustion Phases of Evaporating Neat Fuel Droplet“. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 96, Nr. 1 (06.07.2022): 60–69. http://dx.doi.org/10.37934/arfmts.96.1.6069.
Der volle Inhalt der QuelleDissertationen zum Thema "Two phase flow combustion"
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.
Der volle Inhalt der QuelleSankaran, Vaidyanathan. „Sub-grid Combustion Modeling for Compressible Two-Phase Flows“. Diss., Georgia Institute of Technology, 2003. http://hdl.handle.net/1853/5274.
Der volle Inhalt der QuelleRochette, Bastien. „Modeling and simulation of two-phase flow turbulent combustion in aeronautical engines“. Thesis, Toulouse, INPT, 2019. http://www.theses.fr/2019INPT0059.
Der volle Inhalt der QuelleNowadays, more than 80% of the energy consumed on Earth is produced by burning fossil fuels. Alternative solutions to combustion are being developed but the specific constraints related to air transport do not make it possible to currently power engines without introducing a technological breakthrough. These findings explain the research activity to improve the knowledge and the control of combustion processes to design cleaner, and more efficient aeronautical engines. In this framework, Large Eddy Simulations (LES) have become a powerful tool to better understand combustion processes and pollutant emissions. This PhD thesis is part of this context and focuses on the models and numerical strategies to simulate with more accuracy turbulent gaseous and two-phase reacting flows in the combustion chamber of aeronautical engines. First, a generic and self-adapting method for flame front detection and thickening has been developed for the TFLES model, and validated on several academic configurations of increasing complexity. This generic approach is then evaluated in the LES of a laboratory-scale burner and compared to the classical thickening method. Results show a more accurate thickening in post-flame regions. Second, from the analysis of 1-D homogeneous laminar spray flames where the dispersed phase has a relative velocity compared to the carrier phase, two analytical formulations for the spray flame propagation speed have been proposed and validated. The agreement between the overall trend of both the measured/estimated spray flame speeds demonstrates that the model and its parameters correctly take into account the main physical mechanisms controlling laminar spray flames. Finally, the state-of-the-art TFLES models were tested on complex turbulent gaseous and two-phase reacting configurations. The pros and cons of these models were investigated to contribute to the understanding of the mechanisms related to turbulent combustion, and to propose a LES modeling strategy to improve the fidelity of reactive simulations
Collin, Félix. „Modeling and numerical simulations of two-phase ignition in gas turbine“. Thesis, Toulouse, INPT, 2019. http://www.theses.fr/2019INPT0053.
Der volle Inhalt der QuelleIn order to meet the new international environmental regulations while maintaining a strong economic competitiveness, innovative technologies of aeronautical combustion chambers are developed. These technologies must guarantee fast relight in case of extinction, which is one of the most critical and complex aspects of engine design. Control of this phase involves a thorough understanding of the physical phenomena involved. In this thesis the full two-phase ignition sequence of an aeronautical engine has been studied, from the breakdown of the spark plug to thepropagation of the flame in the complete engine. For this purpose, Large-Eddy Simulations (LES) using a detailed description of the liquid phase (Euler-Lagrange formalism) and of the combustion process (Analytically Reduced Chemistry) were performed. The results also led to the development of a simplified model for the prediction of ignition probability map, which is particularly useful for the design of combustion chambers
Thawley, Scott. „Spatio-temporal Characteristics of a Spray from a Liquid Jet in Crossflow“. Thesis, Virginia Tech, 2006. http://hdl.handle.net/10919/31276.
Der volle Inhalt der QuelleMaster of Science
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.
Der volle Inhalt der QuelleThe energy needs of population around the word are continuously increasing. For instance, forecasts indicates an important grow of the request of the aeronautic transportation sector. It is necessary to continue the research efforts to get more performants and less contaminating systems. New concepts for combustion have been developed and introduced to the gas turbine industry. Among these concepts it is found technologies based on lean-premixed combustion or lean-premixed prevaporized combustion when liquid fuels are employed. These novel energetic systems, making use of lean combustion, are promising to meet the future norms about pollutant emissions, but this make them more sensitive to combustion instabilities that limit their operating range and can lead to irreversible damage. In this domain, many questions still need to be considered. In particular that of the behavior of two-phase flow swirling flames subjected to acoustic perturbations. Indeed most of aero-engines operate with this type of flames, but the dynamics and mutual interaction of these flames, as they are submitted to acoustic perturbation, are not yet well understood. This work addresses these issues and gives some understanding elements for the mechanisms driving the response of the flow and of the flame to acoustic perturbations and delivers data to validate models predicting unstable operating points.The experimental bench employed for this work is TACC-Spray. It has been designed and developed in the CORIA laboratory during this PhD thesis which is inscribed in the framework of the ANR FASMIC project. The injections system that equips this bench is composed by three swirled injectors fed with a liquid fuel (here n-heptane), developed by the EM2C laboratory. They are linearly arranged in the bench such that this represents an unwrapped sector of an annular chamber. The setup, being new and complex, needed technical solutions developed during this work and applied then in order to equip TACC-Spray with pressure and temperature sensors, a photomultiplier as well as adequate optic diagnostics (LDA, PDA, high speed imaging systems). In this study, the energetic system, composed by the two-phase swirling flow and the spray flame, has been submitted to the impact of a transverse acoustic mode excited within the acoustic cavity. The system response has been studied as a function of its location in the acoustic field. Three basins of influence of the acoustic field on the energetic system have been chosen, namely: (i) the pressure antinode characterized mainly by strong pressure fluctuations, (ii) the intensity antinode where important acoustic pressure and velocity gradients are present, (iii) the velocity antinode with strong velocity fluctuations where the acoustic pressure is residual. The approach of the study presented here is to investigate in first place the energetic system free of acoustic forcing. The results concerning this first study are presented in the Part I of this manuscript. In second place, the energetic system is placed in each of the location of interest within the acoustic field and the response of the air flow without combustion, that of the two-phase flow with combustion and finally that of the spray flames, are systematically investigated. The results of the study under acoustic forcing are shown in Part II of the manuscript
Eyssartier, Alexandre. „LES of two-phase reacting flows : stationary and transient operating conditions“. Thesis, Toulouse, INPT, 2012. http://www.theses.fr/2012INPT0011/document.
Der volle Inhalt der QuelleIgnition and altitude reignition are critical issues for aeronautical combustion chambers. The success of ignition depends on multiple factors, from the characteristics of the igniter to the spray droplet size or the level of turbulence at the ignition site. Finding the optimal location of the igniter or the potential of ignition success of a given energy source at a given location are therefore parameters of primary importance in the design of combustion chambers. The purpose of this thesis is to study forced ignition of aeronautical combustion chambers. To do so, Large Eddy Simulations (LES) of two-phase reacting flows are performed and analyzed. First, the equations of the Eulerian formalism used to describe the dispersed phase are presented. To validate the successive LES, experimental data from the MERCATO bench installed at ONERA Fauga-Mauzac are used. It allows to validate the two-phase evaporating flow LES methodology and models prior to its use to other flow conditions. The statistically stationary two-phase flow reacting case is then compared to available data to evaluate the model in reacting conditions. This case is more deeply studied through the analysis of the characteristics of the flame. This last one appears to experience very different combustion regimes. It is also seen that the determination of the most appropriate methodology to compute two-phase flow flame is not obvious. Furthermore, two different methodologies may both agree with the data and still have different burning modes. The ability of the LES to correctly compute burning two-phase flow being validated, LES of the transient ignition phenomena are performed. The experimentally observed sensitivity of ignition to initial conditions, i.e. to sparking time, is recovered with LES. The analysis highlights the major role played by the spray dispersion in the development of the initial flame kernel. The use of LES to compute ignition sequences provides a lot of information about the ignition phenomena, however from an industrial point of view, it does not give an optimal result, unless all locations are tested, which brings the CPU cost to unreasonable values. Alternatives are hence needed and are the objective of the last part of this work. It is proposed to derive a local ignition criterion, giving the probability of ignition from the knowledge of the unsteady non-reacting two-phase (air and fuel) flow. This model is based on criteria for the phases of a successful ignition process, from the first kernel formation to the flame propagation towards the injector. Then, comparisons with experimental data on aeronautical chambers are done and show good agreement, indicating that the proposed ignition criterion, coupled to a Large Eddy Simulation of the stationary evaporating two-phase non-reacting flow, can be used to optimize the igniter location and power
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.
Der volle Inhalt der QuelleAkritopoulos, 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.
Der volle Inhalt der QuelleOverbrüggen, Timo van [Verfasser], Wolfgang [Akademischer Betreuer] Schröder und 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.
Der volle Inhalt der QuelleBücher zum Thema "Two phase flow combustion"
Nguyen, Hung Lee. Two-dimensional analysis of two-phase reacting flow in a firing direct-injection diesel engine. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1989.
Den vollen Inhalt der Quelle findenCenter, Lewis Research, Hrsg. Two-dimensional analysis of two-phase reacting flow in a firing direct-injection diesel engine. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1989.
Den vollen Inhalt der Quelle findenCenter, Lewis Research, Hrsg. Two-dimensional analysis of two-phase reacting flow in a firing direct-injection diesel engine. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1989.
Den vollen Inhalt der Quelle findenI͡Arin, Leonid Petrovich. Osnovy teorii gorenii͡a dvukhfaznykh sred. Leningrad: Ėnergoatomizdat, Leningradskoe otd-nie, 1987.
Den vollen Inhalt der Quelle findenCenter, Lewis Research, Hrsg. LSPRAY: A Lagrangian spray solver, user's manual : prepared under contract NAS3-27186. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.
Den vollen Inhalt der Quelle findenC, Roco M., Hrsg. Particulate two-phase flow. Boston: Butterworth-Heinemann, 1993.
Den vollen Inhalt der Quelle findenYarin, L. P., und G. Hetsroni. Combustion of Two-Phase Reactive Media. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-06299-9.
Der volle Inhalt der QuelleYarin, L. P. Combustion of Two-Phase Reactive Media. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004.
Den vollen Inhalt der Quelle findenYarin, L. P. Combustion of two-phase reactive media. Berlin: Springer, 2004.
Den vollen Inhalt der Quelle findenKakaç, Sadik, Arthur E. Bergles und E. Oliveira Fernandes, Hrsg. Two-Phase Flow Heat Exchangers. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2790-2.
Der volle Inhalt der QuelleBuchteile zum Thema "Two phase flow combustion"
Poinsot, Thierry. „Two-Phase Flow Combustion“. In Instabilities of Flows: With and Without Heat Transfer and Chemical Reaction, 267–85. Vienna: Springer Vienna, 2010. http://dx.doi.org/10.1007/978-3-7091-0127-8_10.
Der volle Inhalt der QuelleCoward, Adrian V., und Philip Hall. „On the Instability of Two-Phase Stagnation Point Flow“. In Transition, Turbulence and Combustion, 181–89. Dordrecht: Springer Netherlands, 1994. http://dx.doi.org/10.1007/978-94-011-1032-7_16.
Der volle Inhalt der QuelleDurst, F., und T. Börner. „Dispersed Two-Phase Flows, its Experimental Investigation and Numerical Prediction“. In Instrumentation for Combustion and Flow in Engines, 295–339. Dordrecht: Springer Netherlands, 1989. http://dx.doi.org/10.1007/978-94-009-2241-9_17.
Der volle Inhalt der QuelleTai, Lv, und Ting-ting Zhou. „Numerical Simulation of Two Phase Flow Characteristic in Dynamic-Static Separator“. In Cleaner Combustion and Sustainable World, 1031–35. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-30445-3_137.
Der volle Inhalt der QuelleDimitrova, D., M. Braun, J. Janicka und 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, 415–44. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-5320-4_14.
Der volle Inhalt der QuelleDiakoumakos, E., J. Anagnostopoulos und G. Bergeles. „A Theoretical Study of Air-Solid Two-Phase Flows“. In Mathematical Modeling in Combustion and Related Topics, 449–59. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2770-4_30.
Der volle Inhalt der QuelleMarchesin, Dan, Jesus da Mota und Aparecido de Souza. „Riemann Solutions for a Model of Combustion in Two-Phase Flow in Porous Media“. In Hyperbolic Problems: Theory, Numerics, Applications, 683–92. Basel: Birkhäuser Basel, 2001. http://dx.doi.org/10.1007/978-3-0348-8372-6_22.
Der volle Inhalt der Quellede Vicente, S., G. Galiano, J. Velasco und 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, 870–76. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-02682-9_135.
Der volle Inhalt der QuelleNguyen, Van Bo, Li Jiun-Ming, Teo Chiang Juay und 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, 397–403. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-46213-4_67.
Der volle Inhalt der QuelleBourgeat, Alain. „Two-Phase Flow“. In Interdisciplinary Applied Mathematics, 95–127. New York, NY: Springer New York, 1997. http://dx.doi.org/10.1007/978-1-4612-1920-0_5.
Der volle Inhalt der QuelleKonferenzberichte zum Thema "Two phase flow combustion"
Hebrard, P., J. Courquet und 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.
Der volle Inhalt der QuelleStowe, R., C. Dubois, P. Harris, A. Mayer, A. De Champlain und S. Ringuette. „Two phase flow combustion modelling of a ducted rocket“. In 37th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3461.
Der volle Inhalt der QuelleMittal, M., und T. Rozmajzl. „Numerical simulation of two-phase fluid flow for combustion“. In 34th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-708.
Der volle Inhalt der QuelleKlose, G., R. Schmehl, R. Meier, G. Meier, R. Koch, S. Wittig, M. Hettel, W. Leuckel und N. Zarzalis. „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.
Der volle Inhalt der QuelleSaha, Kaushik, und 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.
Der volle Inhalt der QuelleLi, Zhaorui, Murat Yaldizli und 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.
Der volle Inhalt der Quellevon Langenthal, Thomas, Nikolaos Zarzalis und 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.
Der volle Inhalt der QuelleYU, F. „Hydraulic analogy application in the study of a two-phase mixture combustion flow“. In 28th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-451.
Der volle Inhalt der QuelleDong, Ming, Maozhao Xie und Hong Liu. „Numerical Study on Turbulent Two-Phase Flow in a Porous Media Combustion Chamber“. In 2008 SAE International Powertrains, Fuels and Lubricants Congress. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2008. http://dx.doi.org/10.4271/2008-01-1592.
Der volle Inhalt der QuelleSrinivasan, Navneeth, Hongyuan Zhang und Suo Yang. „A VLE-Based Reacting Flow Solver for High-Pressure Transcritical Two-Phase Combustion“. In AIAA SCITECH 2023 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-1858.
Der volle Inhalt der QuelleBerichte der Organisationen zum Thema "Two phase flow combustion"
Luke, Gary, Mark Eagar, Michael Sears, Scott Felt und Bob Prozan. Status of Advanced Two-Phase Flow Model Development for SRM Chamber Flow Field and Combustion Modeling. Fort Belvoir, VA: Defense Technical Information Center, Januar 2004. http://dx.doi.org/10.21236/ada427829.
Der volle Inhalt der QuelleCizmas, Paul, und 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), Dezember 2001. http://dx.doi.org/10.2172/792073.
Der volle Inhalt der QuellePaul Cizmas. A REDUCED ORDER MODEL OF TWO-PHASE FLOW, HEAT TRANSFER AND COMBUSTION IN CIRCULATING FLUIDIZED-BEDS. Office of Scientific and Technical Information (OSTI), Dezember 2003. http://dx.doi.org/10.2172/827038.
Der volle Inhalt der QuellePaul Cizmas. A REDUCED ORDER MODEL OF TWO-PHASE FLOW, HEAT TRANSFER AND COMBUSTION IN CIRCULATING FLUIDIZED-BEDS. Office of Scientific and Technical Information (OSTI), Dezember 2002. http://dx.doi.org/10.2172/813624.
Der volle Inhalt der QuelleChapman 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.
Der volle Inhalt der QuelleWallis, G. B. Two phase potential flow. Office of Scientific and Technical Information (OSTI), Juni 1991. http://dx.doi.org/10.2172/6213215.
Der volle Inhalt der QuelleMaeder, P. F., und J. Kestin. Two-phase flow in geothermal systems. Office of Scientific and Technical Information (OSTI), August 1987. http://dx.doi.org/10.2172/5984665.
Der volle Inhalt der QuelleFarwagi, S. M. Computer Modelling of Two-Phase Flow. Fort Belvoir, VA: Defense Technical Information Center, Oktober 1986. http://dx.doi.org/10.21236/ada175048.
Der volle Inhalt der QuelleWallis, G. B. Two-Phase Potential Flow. Final report. Office of Scientific and Technical Information (OSTI), Juni 1999. http://dx.doi.org/10.2172/761114.
Der volle Inhalt der QuelleTheilacker, Jay, und C. Rode. An Investigation Into Flow Regimes for Two Phase Helium Flow. Office of Scientific and Technical Information (OSTI), Oktober 1987. http://dx.doi.org/10.2172/1151469.
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