Книги з теми "Combustion hydrogène"
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Ознайомтеся з топ-50 книг для дослідження на тему "Combustion hydrogène".
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1933-, Wendt Hartmut, ed. Electrochemical hydrogen technologies: Electrochemical production and combustion of hydrogen. Amsterdam: Elsevier, 1990.
Знайти повний текст джерелаEichert, Helmut. Zur Dynamik des Verbrennungsablaufs von Wasserstoff-Luft- und Wasserstoff-Methan-Luft-Gemischen. Koln: DLR, 1989.
Знайти повний текст джерелаGreen, James M. A premixed hydrogen/oxygen catalytic igniter. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Знайти повний текст джерелаGelfand, Boris E., Mikhail V. Silnikov, Sergey P. Medvedev, and 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.
Повний текст джерелаV, Silnikov Mikhail, Medvedev Sergey P, Khomik Sergey V, and SpringerLink (Online service), eds. Thermo-Gas Dynamics of Hydrogen Combustion and Explosion. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.
Знайти повний текст джерелаBillings, Roger E. The hydrogen world view. Independence, Mo: American Academy of Science, 1991.
Знайти повний текст джерелаGerke, Udo. Numerical analysis of mixture formation and combustion in a hydrogen direct-injection internal combustion engine. Göttingen: Cuvillier, 2007.
Знайти повний текст джерелаStamps, 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.
Знайти повний текст джерелаAhuja, J. K. Numerical simulation of shock-induced combustion in a superdetonative hydrogen-air system. Washington, D. C: American Institute of Aeronautics and Astronautics, 1993.
Знайти повний текст джерелаNemitallah, Medhat A., Mohamed A. Habib, and 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.
Повний текст джерелаTamaru, Takashi. Hydrogen fueled subsonic-ram-combustor model tests for an air-turbo-ram engine. Tokyo, Japan: National Aerospace Laboratory, 1990.
Знайти повний текст джерелаSussman, Myles A. A computational study of unsteady shock induced combustion of hydrogen-air mixtures. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.
Знайти повний текст джерелаSzwaja, Stanisław. Studium pulsacji ciśnienia spalania w tłokowym silniku spalinowym zasilanym wodorem. Częstochowa: Wydawn. Politechniki Częstochowskiej, 2010.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. 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.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. 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.
Знайти повний текст джерелаBlanchat, T. K. Deliberate ignition of hydrogen-air-steam mixtures in condensing steam environments. Washington, DC: U.S. Nuclear Regulatory Commission, 1997.
Знайти повний текст джерелаAhuja, J. K. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.
Знайти повний текст джерелаN, Tiwari S., Singh D. J, and Old Dominion University. Dept. of Mechanical Engineering and Mechanics., eds. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Norfolk, Va: Old Dominion University Research Foundation, 1992.
Знайти повний текст джерелаN, Tiwari S., and Langley Research Center, eds. Parametric study of shock-induced combustion in a hydrogen air system. Norfolk, Va: Institute for Computational and Applied Mechanics, Old Dominion University, 1994.
Знайти повний текст джерелаN, Tiwari S., and Langley Research Center, eds. Parametric study of shock-induced combustion in a hydrogen air system. Norfolk, Va: Institute for Computational and Applied Mechanics, Old Dominion University, 1994.
Знайти повний текст джерелаSkyring, R. Experimental determination of hydrogen-air detonation pressure limit and scramjet application. Washington: American Institute of Aeronautics and Astronautics, 1996.
Знайти повний текст джерелаThorne, 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.
Знайти повний текст джерелаDomel, 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.
Знайти повний текст джерелаUnited States. Environmental Protection Agency. Emission Standards Division., ed. 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.
Знайти повний текст джерелаHitch, B. D. Reduced H2-O2 mechanisms for use in reacting flow simulation. New York: AIAA, 1988.
Знайти повний текст джерелаJ, Breisacher Kevin, and United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.
Знайти повний текст джерелаJ, Breisacher Kevin, and United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.
Знайти повний текст джерелаRumminger, 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.
Знайти повний текст джерелаWong, 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.
Знайти повний текст джерелаL, Olson Sandra, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. 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.
Знайти повний текст джерелаL, Olson Sandra, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. 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.
Знайти повний текст джерелаN, Tiwari S., and United States. National Aeronautics and Space Administration, eds. 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.
Знайти повний текст джерелаN, Tiwari S., and United States. National Aeronautics and Space Administration., eds. 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.
Знайти повний текст джерелаHuang, Morren Sybil, and United States. National Aeronautics and Space Administration., eds. A Laboratory model of a hydrogen/oxygen engine for combustion and nozzle studies. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Знайти повний текст джерелаR, Tieszen S., Benedick William B, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Systems Research., and Sandia National Laboratories, eds. 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.
Знайти повний текст джерелаKanilo, P. M. Ėnergeticheskie i ėkologicheskie kharakteristiki GTD pri ispolʹzovanii uglevodorodnykh topliv i vodoroda. Kiev: Nauk. dumka, 1987.
Знайти повний текст джерелаD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.), and Building and Fire Research Laboratory (U.S.), eds. 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.
Знайти повний текст джерелаD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.), and Building and Fire Research Laboratory (U.S.), eds. 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.
Знайти повний текст джерелаD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.), and Building and Fire Research Laboratory (U.S.), eds. 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.
Знайти повний текст джерелаR, Thomas S., and United States. National Aeronautics and Space Administration., eds. Numerical study of contaminant effects on combustion of hydrogen, ethane and methane in air. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.), and Building and Fire Research Laboratory (U.S.), eds. 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.
Знайти повний текст джерелаD, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.), and Building and Fire Research Laboratory (U.S.), eds. 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.
Знайти повний текст джерелаRosa, 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.
Знайти повний текст джерелаRosa, 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.
Знайти повний текст джерелаU.S. Nuclear Regulatory Commission. Office of Nuclear Reactor Regulation. Division of Engineering and System Technology. and Sandia National Laboratories, eds. 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.
Знайти повний текст джерелаJ, Schneider Steven, and United States. National Aeronautics and Space Administration., eds. Testing of wrought iridium/chemical vapor deposition rhenium rocket. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаJ, Schneider Steven, and United States. National Aeronautics and Space Administration., eds. Testing of wrought iridium/chemical vapor deposition rhenium rocket. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаM, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаM, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаM, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
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