Auswahl der wissenschaftlichen Literatur zum Thema „Liquid oxygen and methane“
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Zeitschriftenartikel zum Thema "Liquid oxygen and methane"
Oh, Choeulwoo, und Hyung-Suk Oh. „Confined Oxygen Promotes Radical Generation for Methane Oxidation Toward Liquid Oxygenates“. ECS Meeting Abstracts MA2022-02, Nr. 49 (09.10.2022): 1915. http://dx.doi.org/10.1149/ma2022-02491915mtgabs.
Der volle Inhalt der QuelleUrzica, Daniela, und Eva Gutheil. „Structures of Laminar Methane/Nitrogen/Oxygen, Methane/Oxygen and Methane/Liquid Oxygen Counterflow Flames for Cryogenic Conditions and Elevated Pressures“. Zeitschrift für Physikalische Chemie 223, Nr. 4-5 (Mai 2009): 651–67. http://dx.doi.org/10.1524/zpch.2009.6050.
Der volle Inhalt der QuelleRicci, Daniele, Francesco Battista und Manrico Fragiacomo. „Transcritical Behavior of Methane in the Cooling Jacket of a Liquid-Oxygen/Liquid-Methane Rocket-Engine Demonstrator“. Energies 15, Nr. 12 (07.06.2022): 4190. http://dx.doi.org/10.3390/en15124190.
Der volle Inhalt der QuelleXu, Zhen Chao, und Eun Duck Park. „Gas-Phase Selective Oxidation of Methane into Methane Oxygenates“. Catalysts 12, Nr. 3 (09.03.2022): 314. http://dx.doi.org/10.3390/catal12030314.
Der volle Inhalt der QuelleMariyana, Rina, Min-Sik Kim, Chae Lim, Tae Kim, Si Park, Byung-Keun Oh, Jinwon Lee und Jeong-Geol Na. „Mass Transfer Performance of a String Film Reactor: A Bioreactor Design for Aerobic Methane Bioconversion“. Catalysts 8, Nr. 11 (24.10.2018): 490. http://dx.doi.org/10.3390/catal8110490.
Der volle Inhalt der QuelleThu, Vu Phuong. „COMBINATION OF METHANE OXIDATION AND DENITRIFICATION PROCESS IN A TWO-STAGE BIOREACTOR“. Vietnam Journal of Science and Technology 54, Nr. 4B (22.03.2018): 27. http://dx.doi.org/10.15625/2525-2518/54/4b/12020.
Der volle Inhalt der QuelleHaranguş, Victoria, Gabriel Vasilescu, Adela Todoruţ und Teodor Hepuţ. „Analysis of Hazards Identified within the Premises of the Electric Steelworks, to Carry out the Risk Assessment“. Solid State Phenomena 216 (August 2014): 97–102. http://dx.doi.org/10.4028/www.scientific.net/ssp.216.97.
Der volle Inhalt der QuelleKočí, Kamila, Lucie Obalová, Daniela Plachá und Zdenek Lacný. „Effect of Temperature, Pressure and Volume of Reacting Phase on Photocatalytic CO2 Reduction on Suspended Nanocrystalline TiO2“. Collection of Czechoslovak Chemical Communications 73, Nr. 8-9 (2008): 1192–204. http://dx.doi.org/10.1135/cccc20081192.
Der volle Inhalt der QuelleStevenson, James, Jonathan Lunine und Paulette Clancy. „Membrane alternatives in worlds without oxygen: Creation of an azotosome“. Science Advances 1, Nr. 1 (Februar 2015): e1400067. http://dx.doi.org/10.1126/sciadv.1400067.
Der volle Inhalt der QuelleKang, Jongkyu, und Eun Duck Park. „Selective Oxidation of Methane over Fe-Zeolites by In Situ Generated H2O2“. Catalysts 10, Nr. 3 (05.03.2020): 299. http://dx.doi.org/10.3390/catal10030299.
Der volle Inhalt der QuelleDissertationen zum Thema "Liquid oxygen and methane"
Lechner, Valentin. „Experimental study of LOX/CH4 flames in rocket engines“. Electronic Thesis or Diss., université Paris-Saclay, 2024. http://www.theses.fr/2024UPAST040.
Der volle Inhalt der QuelleUsing methane as a fuel in rocket engines would have many advantages but the combustion with pure oxygen at high pressure remains poorly understood. From a thermodynamic point of view, methane and oxygen share very similar critical point values, making it challenging to predict propellant mixing, flame anchoring, stability and structure. Moreover, when methane is injected in excess, aerosols can be produced, which can clog the lines, damage the turbine, and reduce the efficiency.Therefore, a thorough update of the knowledge of LOX/CH4 combustion is necessary. These challenges are tackled within the consortium composed of EM2C laboratory, ONERA, CNES, and ArianeGroup. Two test campaigns are carried out at the MASCOTTE facility from ONERA, aiming to study three central topics: the flame structure, wall heat transfers, and aerosol production. To this end, various experimental diagnostics are implemented simultaneously during high-pressure hot-fire tests.Various imaging diagnostics are implemented to analyze the flame structure and the dense liquid jets. Despite the acquisition difficulties encountered in these extreme conditions, the analyses reveal a complex flame structure. In the subcritical regime, atomization and evaporation mechanisms dominate. The flame is much more opened and longer than at higher pressures, where diffusive mixing mechanisms prevail. Characterizing flame anchoring remains a challenge. A water ice ring surrounding, and masking, the flame foot has been identified. Formation mechanisms are proposed, and a growth/destruction temporal cycle is highlighted. Its presence strongly affects flame visualizations, and may lead to misinterpretations of its topology.Laser-induced phosphorescence (LIP) is implemented for the first time at MASCOTTE. Various LIP methods exist, but they are not well suited to the MASCOTTE conditions: wide temperature range, thermal transients, and two-phase flow environment favoring laser absorption/diffusion. Therefore, a specific method, the Full Spectrum Fitting method (FSF method), has been developed. It exploits the spectral dependence on temperature, enabling instantaneous measurements from 100 to 900 K with a precision of 17 K, with no dependence on the laser excitation energy. A detailed data analysis highlights the predominant wall heat transfer modes, studies the influence of the operating points, and compares the experimental data with a wall heat transfer model, which is particularly well suited for deducing the convective properties of the flow.Three diagnostics are used to characterize aerosols. An intrusive probe samples particles and burnt gases downstream of the flame. The particles are sampled on TEM grids and analyzed by Transmission Electron Microscopy. Detailed images of the aerosol morphology reveal that the particles are soot. Combustion products are analyzed by gas chromatography. This makes it possible to identify soot precursor molecules such as benzene and acetylene. Soot are quantified temporally by laser extinction. A dedicated post-processing method is developed and various hypotheses are discussed to explain the spatial variations of the soot production downstream of the flame
Hartwig, Jason W. „Liquid Acquisition Devices for Advanced In-Space Cryogenic Propulsion Systems“. Case Western Reserve University School of Graduate Studies / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=case1396562473.
Der volle Inhalt der QuelleSalusbury, Sean. „Premixed methane stagnation flames with oxygen enrichment“. Thesis, McGill University, 2010. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=87008.
Der volle Inhalt der QuelleThe experimental apparatus that is used to gather data in this study is a stagnation flame burner. Particle image velocimetry, a laser-based flow visualization technique, is used to measure velocity in both the axial and radial directions. The results are analyzed first to confirm the validity of the one-dimensional, axisymmetric model commonly used to describe impinging-jet flow. Experimental results are found to have good agreement with theoretical approximations and numerical models. Tests are then conducted to reproduce previously published data for methane-air flames at lean, stoichiometric and rich conditions in order to prove the reliability of the experimental apparatus. There is agreement between published data and the new experimental results.
Experiments with oxygen enrichment are then conducted at equivalence ratios not normally within the flammability limits of methane-air mixtures, from the very lean, phi = 0.55, to the very rich, phi = 1.45. Results show marked disagreement between model and experiment at equivalence ratios far from stoichiometric. These experimental data will allow the chemical kinetic model for premixed methane combustion to be improved -- by correcting divergence in the model at very lean and very rich conditions, the model should be improved appreciably over the narrower range of equivalence ratios typically seen in methane-air combustion.
La cinétique chimique est la science de la modélisation des étapes d'une réaction chimique au niveau moléculaire. Ce mémoire s'interesse aux réactions chimique qui se produisent durant la combustion. Les modèles cinétique présentement acceptés sont en besoin d'amélioration et d'autres enplus, il existe plusieurs réactions qui n'ont aucun modèle. Pour mieux développer les modèles et pour en créer des nouveaux, il fault rassembler assez de données expérimentales pour produire une base solide sur laquelle des modèles de plus en plus compliqués peuvent etre construits.
Pour générer des données, cette étude utilise un appareil expérimental avec une géométrie de point d'arrêt, dans laquelle une flamme aplatie peut exister. Les vitesses dans la direction axiale et radiale sont mesurées par la vélocimétire image-particule, une technique à base de laser. Les résultats sont d'abord analisés pour vérifier que le modèle unidimensionnel est valide. Une bonne concordance est observée entre la théorie et les résultats et entre les modèles numériques et les résultats. Subséquemment, des expériences sont effectuées pour reproduire des données déjà publiées pour le méthane et l'air aux rapports d'équivalence oxydants, stoechiométriques et réducteurs, afin de prouver la fiabilité de l'appareil expérimental. Il ya une bonne concordance entre les données publiées et les résultats expérimentaux.
Des expériences dans lequelles l'air est enrichi avec de l'oxygène sont effectuées à des rapports d'équivalence de phi = 0.55 juste qu'à phi = 1.45; ces rapports d'équivalence ne sont normalement pas dans les limites d'inflammabilité des mélanges de méthane-air. Ici, les résultats montrent un désaccord marqué entre le modèle et les expériences pour les rapports d'équivalence très loin de phi = 1.0. Les données permettent le modèle cinétique chimique pour la combustion du méthane prémélangée d'être amélioré. En corrigeant les divergences entre le modèle et les resultats experimentales pour rapports d'équivalence très oxydants et très réducteurs, le modèle sera amélioré pour rapports d'équivalences généralement vus dans la combusiton de méthane dans l'air.
Williams, Gareth Richard. „Liquid phase catalytic partial oxidation of methane“. Thesis, University of Bath, 2002. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.760824.
Der volle Inhalt der QuellePedersen, Tom. „A study of liquid film, liquid motion, and oxygen absorption from hemispherical air/oxygen bubbles“. Thesis, Brunel University, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.242980.
Der volle Inhalt der QuelleWishnow, Edward Hyman. „Far-infrared absorption by liquid nitrogen and liquid oxygen“. Thesis, University of British Columbia, 1985. http://hdl.handle.net/2429/25072.
Der volle Inhalt der QuelleScience, Faculty of
Physics and Astronomy, Department of
Graduate
Teeple, Brian S. (Brian Scott). „Feasibility of producing lunar liquid oxygen“. Thesis, Massachusetts Institute of Technology, 1994. http://hdl.handle.net/1721.1/47360.
Der volle Inhalt der QuelleLee, Colleen Su-Ming. „Reactions of oxygen with methane using microwave and conventional heating“. Thesis, Imperial College London, 2000. http://hdl.handle.net/10044/1/8073.
Der volle Inhalt der QuelleRivera-Rivera, Ramiro Luis. „Simulation and validation of liquid oxygen and liquid hydrogen pressurization systems“. Thesis, Available online, Georgia Institute of Technology, 2004:, 2003. http://etd.gatech.edu/theses/available/etd-04072004-180151/unrestricted/rivera-rivera%5Framiro%5Fl%5F200312%5Fms.pdf.
Der volle Inhalt der QuelleAgarwal, Nishtha. „Low temperature selective oxidation of methane using hydrogen peroxide and oxygen“. Thesis, Cardiff University, 2018. http://orca.cf.ac.uk/117851/.
Der volle Inhalt der QuelleBücher zum Thema "Liquid oxygen and methane"
J, Nowobilski J., und Lewis Research Center, Hrsg. Airborne rotary air separator study: Final report. Tonawanda, NY: Praxair, Inc., 1992.
Den vollen Inhalt der Quelle findenMoore, Steve. Liquid oxygen. Newcastle upon Tyne: Echo Room Press, 1998.
Den vollen Inhalt der Quelle findenLaw, Susan. Liquid oxygen therapy at home. Montréal, QC: Agence d'évaluation des technologies et des modes d'intervention en santé, 2005.
Den vollen Inhalt der Quelle findenZuckerwar, Allan J. Sound speed measurements in liquid oxygen-liquid nitrogen mixtures. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Den vollen Inhalt der Quelle findenA, Santavicca Domenic, und United States. National Aeronautics and Space Administration., Hrsg. Laser induced spark ignition of methane-oxygen mixtures. [Washington, D.C.?: National Aeronautics and Space Administration, 1991.
Den vollen Inhalt der Quelle findenShapiro, Wilbur. Sealing technology for liquid oxygen (LOX) turbopumps. [Washington, DC: National Aeronautics and Space Administration, 1988.
Den vollen Inhalt der Quelle findenE, Edwards, Hrsg. Composition of the vapour and liquid phases of the system methane nitrogen. [Toronto]: University library, pub. by the Librarian, 1996.
Den vollen Inhalt der Quelle findenArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. [Washington, D.C.]: NASA, 1990.
Den vollen Inhalt der Quelle findenZuckerwar, Allan J. Contamination of liquid oxygen by pressurized gaseous nitrogen. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Tachnical Information Division, 1989.
Den vollen Inhalt der Quelle findenArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. [Washington, D.C.]: NASA, 1990.
Den vollen Inhalt der Quelle findenBuchteile zum Thema "Liquid oxygen and methane"
Winkelmann, J. „Diffusion of methane (1); oxygen (2)“. In Gases in Gases, Liquids and their Mixtures, 815. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-49718-9_533.
Der volle Inhalt der QuelleWinkelmann, J. „Diffusion of methane (1); oxygen (2)“. In Gases in Gases, Liquids and their Mixtures, 228. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-49718-9_76.
Der volle Inhalt der QuelleWinkelmann, J. „Diffusion of oxygen (1); tetrachloro-methane (2)“. In Gases in Gases, Liquids and their Mixtures, 2087. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-49718-9_1604.
Der volle Inhalt der QuelleFeng, Lei, Wen Chen, Jingrun Wang, Wen Xie, Qingxin Cui, Jingying Bai und Cheng’an Wan. „Research on Space Regenerative Fuel Cell System and Comprehensive Energy Utilization Technology“. In Proceedings of the 10th Hydrogen Technology Convention, Volume 1, 334–43. Singapore: Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-99-8631-6_32.
Der volle Inhalt der QuelleWinkelmann, J. „Diffusion of dichloro-difluoro-methane (1); oxygen (2)“. In Gases in Gases, Liquids and their Mixtures, 762. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-49718-9_486.
Der volle Inhalt der QuelleWinkelmann, J. „Diffusion of chloro-difluoro-methane (1); oxygen (2)“. In Gases in Gases, Liquids and their Mixtures, 780. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-49718-9_502.
Der volle Inhalt der QuelleSong, Hui. „Direct Photocatalytic Oxidation of Methane to Liquid Oxygenates with Molecular Oxygen over Nanometals/ZnO Catalysts“. In Solar-Energy-Mediated Methane Conversion Over Nanometal and Semiconductor Catalysts, 93–117. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-33-4157-9_5.
Der volle Inhalt der QuelleCampbell, K. D., H. Zhang und J. H. Lunsford. „Methane Activation Over Lanthanide Oxides“. In Oxygen Complexes and Oxygen Activation by Transition Metals, 308. Boston, MA: Springer US, 1988. http://dx.doi.org/10.1007/978-1-4613-0955-0_23.
Der volle Inhalt der QuelleLunsford, J. H. „Methane Oxidation at Metal Oxide Surfaces“. In Oxygen Complexes and Oxygen Activation by Transition Metals, 265–72. Boston, MA: Springer US, 1988. http://dx.doi.org/10.1007/978-1-4613-0955-0_19.
Der volle Inhalt der QuelleWinkelmann, J. „Diffusion of oxygen (1); water (2); methanol (3)“. In Gases in Gases, Liquids and their Mixtures, 2253. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-49718-9_1743.
Der volle Inhalt der QuelleKonferenzberichte zum Thema "Liquid oxygen and methane"
DeLong, Dan, Jeff Greason und Khaki Rodway McKee. „Liquid Oxygen/Liquid Methane Rocket Engine Development“. In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2007. http://dx.doi.org/10.4271/2007-01-3876.
Der volle Inhalt der QuelleNilsen, Christopher, Scott Meyer und Silas Meriam. „Purdue Liquid Oxygen - Liquid Methane Sounding Rocket“. In AIAA Scitech 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-0614.
Der volle Inhalt der QuelleFlynn, Howard, Brian Lusby und Mark Villemarette. „Liquid Oxygen/Liquid Methane Integrated Propulsion System Test Bed“. In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-5842.
Der volle Inhalt der QuelleBostwick, Christopher, Tristan Gibbs und Eric Besnard. „Liquid Oxygen / Liquid Methane Co-Axial Swirl Injector Development“. In 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-6666.
Der volle Inhalt der QuelleTruong, Colby, Ethan Sichler, Andre H. Lam, Richard Picard und Frank O. Chandler. „Development of a Liquid Oxygen / Liquid Methane Rocket Engine Injector“. In 2018 Joint Propulsion Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4762.
Der volle Inhalt der QuelleMarshall, William, Sibtosh Pal, Roger Woodward und Robert Santoro. „Combustion Instability Studies Using Gaseous Methane and Liquid Oxygen“. In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-4526.
Der volle Inhalt der QuelleHerrera, Manuel, Mariana Chaidez, Zachary Welsh, Jason Adams, Luz I. Bugarin, Jack Chessa und Ahsan R. Choudhuri. „Design and Testing of a 500 lbf Liquid Oxygen/Liquid Methane Engine“. In AIAA Propulsion and Energy 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-3937.
Der volle Inhalt der QuelleHerrera, Manuel, Marissa B. Garcia, Jason Adams, Ahsan R. Choudhuri und Jack Chessa. „Design and Development of a 500 lbf Liquid Oxygen/Liquid Methane Engine“. In 2018 Joint Propulsion Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4605.
Der volle Inhalt der QuelleTrinh, Huu. „Liquid methane/oxygen injector study for potential future Mars ascent“. In 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-3119.
Der volle Inhalt der QuelleMüller, H., und M. Pfitzner. „Large-eddy simulation of transcritical liquid oxygen/methane jet flames“. In Progress in Propulsion Physics – Volume 11. Les Ulis, France: EDP Sciences, 2019. http://dx.doi.org/10.1051/eucass/201911177.
Der volle Inhalt der QuelleBerichte der Organisationen zum Thema "Liquid oxygen and methane"
Egbert, Scott, Xuefang Li, Myra L. Blaylock und Ethan Hecht. Mixing of Liquid Methane Releases. Office of Scientific and Technical Information (OSTI), Dezember 2018. http://dx.doi.org/10.2172/1488323.
Der volle Inhalt der QuellePetrovic, S., A. R. Sanger, P. Komorowski, J. Leman, R. Willier, S. Thind, S. Donini, J. Galuszka und P. Chantal. Electrochemical methane coupling in the absence of oxygen. Natural Resources Canada/ESS/Scientific and Technical Publishing Services, 1994. http://dx.doi.org/10.4095/305317.
Der volle Inhalt der QuelleWarren, B. K., K. D. Campbell und J. L. Matherne. Direct conversion of methane to C sub 2 's and liquid fuels. Office of Scientific and Technical Information (OSTI), Februar 1990. http://dx.doi.org/10.2172/6307190.
Der volle Inhalt der QuelleWarren, B. K., und K. D. Campbell. Direct conversion of methane to C sub 2 's and liquid fuels. Office of Scientific and Technical Information (OSTI), November 1989. http://dx.doi.org/10.2172/6166436.
Der volle Inhalt der QuelleWarren, B. K., K. D. Campbell, J. L. Matherne und N. E. Kinkade. Direct conversion of methane to C sub 2 's and liquid fuels. Office of Scientific and Technical Information (OSTI), März 1990. http://dx.doi.org/10.2172/6166447.
Der volle Inhalt der QuelleWarren, B., K. Campbell, J. Matherne, G. Culp und N. Kinkade. Direct conversion of methane to C sub 2 's and liquid fuels. Office of Scientific and Technical Information (OSTI), April 1990. http://dx.doi.org/10.2172/6203907.
Der volle Inhalt der QuelleMountain, R. D. Molecular dynamics study of the solubility of oxygen in liquid pyridine. Gaithersburg, MD: National Institute of Standards and Technology, 2003. http://dx.doi.org/10.6028/nist.ir.7075.
Der volle Inhalt der QuelleChein, Tsan-Heui, Jin Wei und Yonhua Tzeng. Synthesis of Diamond in High Power-Density Microwave Methane/Hydrogen/Oxygen Plasmas at Elevated Substrate Temperatures. Fort Belvoir, VA: Defense Technical Information Center, April 1999. http://dx.doi.org/10.21236/ada362769.
Der volle Inhalt der QuelleStapelmann, Katharina. Final Report: Absolute Reactive Oxygen Species Densities in the Effluent of the COST Reference Source and Plasma-generated Atomic Oxygen Density Measurements in Liquid using TALIF. Office of Scientific and Technical Information (OSTI), Februar 2024. http://dx.doi.org/10.2172/2309756.
Der volle Inhalt der QuelleHamilton, D. C. Electrical conductivity and equation of state of liquid nitrogen, oxygen, benzene, and 1-butene shocked to 60 GPa. Office of Scientific and Technical Information (OSTI), Oktober 1986. http://dx.doi.org/10.2172/7260956.
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