Bücher zum Thema „Combustion hydrogène“
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1933-, Wendt Hartmut, Hrsg. Electrochemical hydrogen technologies: Electrochemical production and combustion of hydrogen. Amsterdam: Elsevier, 1990.
Den vollen Inhalt der Quelle findenEichert, Helmut. Zur Dynamik des Verbrennungsablaufs von Wasserstoff-Luft- und Wasserstoff-Methan-Luft-Gemischen. Koln: DLR, 1989.
Den vollen Inhalt der Quelle findenGreen, James M. A premixed hydrogen/oxygen catalytic igniter. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Den vollen Inhalt der Quelle findenGelfand, Boris E., Mikhail V. Silnikov, Sergey P. Medvedev und Sergey V. Khomik. Thermo-Gas Dynamics of Hydrogen Combustion and Explosion. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-25352-2.
Der volle Inhalt der QuelleV, Silnikov Mikhail, Medvedev Sergey P, Khomik Sergey V und SpringerLink (Online service), Hrsg. Thermo-Gas Dynamics of Hydrogen Combustion and Explosion. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.
Den vollen Inhalt der Quelle findenBillings, Roger E. The hydrogen world view. Independence, Mo: American Academy of Science, 1991.
Den vollen Inhalt der Quelle findenGerke, Udo. Numerical analysis of mixture formation and combustion in a hydrogen direct-injection internal combustion engine. Göttingen: Cuvillier, 2007.
Den vollen Inhalt der Quelle findenStamps, D. W. Hydrogen-air-diluent detonation study for nuclear reactor safety analyses. Washington, D.C: Division of Systems Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1991.
Den vollen Inhalt der Quelle findenAhuja, J. K. Numerical simulation of shock-induced combustion in a superdetonative hydrogen-air system. Washington, D. C: American Institute of Aeronautics and Astronautics, 1993.
Den vollen Inhalt der Quelle findenNemitallah, Medhat A., Mohamed A. Habib und Ahmed Abdelhafez. Hydrogen for Clean Energy Production: Combustion Fundamentals and Applications. Singapore: Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-7925-3.
Der volle Inhalt der QuelleTamaru, Takashi. Hydrogen fueled subsonic-ram-combustor model tests for an air-turbo-ram engine. Tokyo, Japan: National Aerospace Laboratory, 1990.
Den vollen Inhalt der Quelle findenSussman, Myles A. A computational study of unsteady shock induced combustion of hydrogen-air mixtures. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.
Den vollen Inhalt der Quelle findenSzwaja, Stanisław. Studium pulsacji ciśnienia spalania w tłokowym silniku spalinowym zasilanym wodorem. Częstochowa: Wydawn. Politechniki Częstochowskiej, 2010.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. An analytical study of the hydrogen-air reaction mechanism with application to scramjet combustion. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. An analytical study of the hydrogen-air reaction mechanism with application to scramjet combustion. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Den vollen Inhalt der Quelle findenBlanchat, T. K. Deliberate ignition of hydrogen-air-steam mixtures in condensing steam environments. Washington, DC: U.S. Nuclear Regulatory Commission, 1997.
Den vollen Inhalt der Quelle findenAhuja, J. K. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.
Den vollen Inhalt der Quelle findenN, Tiwari S., Singh D. J und Old Dominion University. Dept. of Mechanical Engineering and Mechanics., Hrsg. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Norfolk, Va: Old Dominion University Research Foundation, 1992.
Den vollen Inhalt der Quelle findenN, Tiwari S., und Langley Research Center, Hrsg. Parametric study of shock-induced combustion in a hydrogen air system. Norfolk, Va: Institute for Computational and Applied Mechanics, Old Dominion University, 1994.
Den vollen Inhalt der Quelle findenN, Tiwari S., und Langley Research Center, Hrsg. Parametric study of shock-induced combustion in a hydrogen air system. Norfolk, Va: Institute for Computational and Applied Mechanics, Old Dominion University, 1994.
Den vollen Inhalt der Quelle findenSkyring, R. Experimental determination of hydrogen-air detonation pressure limit and scramjet application. Washington: American Institute of Aeronautics and Astronautics, 1996.
Den vollen Inhalt der Quelle findenThorne, L. R. Platinum catalytic igniters for lean hydrogen-air mixtures. Washington, DC: Division of Engineering, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1988.
Den vollen Inhalt der Quelle findenDomel, N. D. A two-dimensional numerical simulation of shock-enhanced mixing in a rectangular scramjet flowfield with parallel hydrogen injection. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.
Den vollen Inhalt der Quelle findenUnited States. Environmental Protection Agency. Emission Standards Division., Hrsg. Basis and purpose document on specifications for hydrogen-fueled flares. Research Triangle Park, N.C: U.S. Environmental Protection Agency, Office of Air [and] Radiation, Office of Air Quality Planning [and] Standards, 1998.
Den vollen Inhalt der Quelle findenHitch, B. D. Reduced H2-O2 mechanisms for use in reacting flow simulation. New York: AIAA, 1988.
Den vollen Inhalt der Quelle findenJ, Breisacher Kevin, und United States. National Aeronautics and Space Administration., Hrsg. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.
Den vollen Inhalt der Quelle findenJ, Breisacher Kevin, und United States. National Aeronautics and Space Administration., Hrsg. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.
Den vollen Inhalt der Quelle findenRumminger, Marc D. Inhibition of premixed carbon monoxide-hydrogen-oxygen-nitrogen flames by iron pentacarbonyl. Gaithersburg, Md: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.
Den vollen Inhalt der Quelle findenWong, Chung-Nin Channy. HECTR analyses of the Nevada Test Site (NTS) premixed combustion experiments. Washington, DC: Division of Systems Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1988.
Den vollen Inhalt der Quelle findenL, Olson Sandra, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Hrsg. Fuel-rich catalytic combustion: A soot-free technique for in situ hydrogen-like enrichment. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Den vollen Inhalt der Quelle findenL, Olson Sandra, und United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., Hrsg. Fuel-rich catalytic combustion: A soot-free technique for in situ hydrogen-like enrichment. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Den vollen Inhalt der Quelle findenN, Tiwari S., und United States. National Aeronautics and Space Administration, Hrsg. Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations. Norfolk, Va: Dept. of Chemical Sciences, College of Sciences, Old Dominion University, 1986.
Den vollen Inhalt der Quelle findenN, Tiwari S., und United States. National Aeronautics and Space Administration., Hrsg. Numerical study of hydrogen-air supersonic combustion by using elliptic and parabolized equations. Norfolk, Va: Dept. of Chemical Sciences, College of Sciences, Old Dominion University, 1986.
Den vollen Inhalt der Quelle findenHuang, Morren Sybil, und United States. National Aeronautics and Space Administration., Hrsg. A Laboratory model of a hydrogen/oxygen engine for combustion and nozzle studies. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Den vollen Inhalt der Quelle findenR, Tieszen S., Benedick William B, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Systems Research. und Sandia National Laboratories, Hrsg. FLAME facility: The effect of obstacles and transverse venting on flame acceleration and transition to detonation for hydrogen-air mixtures at large scale. Washington, DC: Division of Systems Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1989.
Den vollen Inhalt der Quelle findenKanilo, P. M. Ėnergeticheskie i ėkologicheskie kharakteristiki GTD pri ispolʹzovanii uglevodorodnykh topliv i vodoroda. Kiev: Nauk. dumka, 1987.
Den vollen Inhalt der Quelle findenD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) und Building and Fire Research Laboratory (U.S.), Hrsg. Premixed carbon monoxide-nitrous oxide-hydrogen flames: Measured and calculated burning velocities with and without Fe(CO)₅. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.
Den vollen Inhalt der Quelle findenD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) und Building and Fire Research Laboratory (U.S.), Hrsg. Premixed carbon monoxide-nitrous oxide-hydrogen flames: Measured and calculated burning velocities with and without Fe(CO)₅. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.
Den vollen Inhalt der Quelle findenD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) und Building and Fire Research Laboratory (U.S.), Hrsg. Premixed carbon monoxide-nitrous oxide-hydrogen flames: Measured and calculated burning velocities with and without Fe(CO)₅. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.
Den vollen Inhalt der Quelle findenR, Thomas S., und United States. National Aeronautics and Space Administration., Hrsg. Numerical study of contaminant effects on combustion of hydrogen, ethane and methane in air. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) und Building and Fire Research Laboratory (U.S.), Hrsg. Premixed carbon monoxide-nitrous oxide-hydrogen flames: Measured and calculated burning velocities with and without Fe(CO)b5s. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.
Den vollen Inhalt der Quelle findenD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) und Building and Fire Research Laboratory (U.S.), Hrsg. Premixed carbon monoxide-nitrous oxide-hydrogen flames: Measured and calculated burning velocities with and without Fe(CO)b5s. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1999.
Den vollen Inhalt der Quelle findenRosa, Maria I. De. Embedded hydrogen chloride and smoke particle characteristics during combustion of polyvinyl chloride and chlorinated mine materials. Washington, D.C: U.S. Dept. of the Interior, Bureau of Mines, 1991.
Den vollen Inhalt der Quelle findenRosa, Maria I. De. Embedded hydrogen chloride and smoke particle characteristics during combustion of polyvinyl chloride and chlorinated mine materials. Washington, DC: U.S. Dept. of the Interior, Bureau of Mines, 1990.
Den vollen Inhalt der Quelle findenU.S. Nuclear Regulatory Commission. Office of Nuclear Reactor Regulation. Division of Engineering and System Technology. und Sandia National Laboratories, Hrsg. Experimental results pertaining to the performance of thermal igniters. Washington, DC: Division of Engineering and Systems Technology, Office of Nuclear Reactor Regulation, U.S. Nuclear Regulatory Commission, 1989.
Den vollen Inhalt der Quelle findenJ, Schneider Steven, und United States. National Aeronautics and Space Administration., Hrsg. Testing of wrought iridium/chemical vapor deposition rhenium rocket. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenJ, Schneider Steven, und United States. National Aeronautics and Space Administration., Hrsg. Testing of wrought iridium/chemical vapor deposition rhenium rocket. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Den vollen Inhalt der Quelle findenM, Kazaroff John, Jankovsky Robert S und United States. National Aeronautics and Space Administration., Hrsg. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Den vollen Inhalt der Quelle findenM, Kazaroff John, Jankovsky Robert S und United States. National Aeronautics and Space Administration., Hrsg. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Den vollen Inhalt der Quelle findenM, Kazaroff John, Jankovsky Robert S und United States. National Aeronautics and Space Administration., Hrsg. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
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