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Livros sobre o tema "Combustion hydrogène"

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1

1933-, Wendt Hartmut, ed. Electrochemical hydrogen technologies: Electrochemical production and combustion of hydrogen. Amsterdam: Elsevier, 1990.

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2

Eichert, Helmut. Zur Dynamik des Verbrennungsablaufs von Wasserstoff-Luft- und Wasserstoff-Methan-Luft-Gemischen. Koln: DLR, 1989.

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3

Green, James M. A premixed hydrogen/oxygen catalytic igniter. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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4

Gelfand, Boris E., Mikhail V. Silnikov, Sergey P. Medvedev e 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.

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5

V, Silnikov Mikhail, Medvedev Sergey P, Khomik Sergey V e SpringerLink (Online service), eds. Thermo-Gas Dynamics of Hydrogen Combustion and Explosion. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012.

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6

Billings, Roger E. The hydrogen world view. Independence, Mo: American Academy of Science, 1991.

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7

Gerke, Udo. Numerical analysis of mixture formation and combustion in a hydrogen direct-injection internal combustion engine. Göttingen: Cuvillier, 2007.

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8

Stamps, 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.

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9

Ahuja, J. K. Numerical simulation of shock-induced combustion in a superdetonative hydrogen-air system. Washington, D. C: American Institute of Aeronautics and Astronautics, 1993.

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10

Nemitallah, Medhat A., Mohamed A. Habib e 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.

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11

Tamaru, Takashi. Hydrogen fueled subsonic-ram-combustor model tests for an air-turbo-ram engine. Tokyo, Japan: National Aerospace Laboratory, 1990.

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12

Sussman, Myles A. A computational study of unsteady shock induced combustion of hydrogen-air mixtures. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.

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13

Szwaja, Stanisław. Studium pulsacji ciśnienia spalania w tłokowym silniku spalinowym zasilanym wodorem. Częstochowa: Wydawn. Politechniki Częstochowskiej, 2010.

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14

United 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.

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15

United 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.

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16

Blanchat, T. K. Deliberate ignition of hydrogen-air-steam mixtures in condensing steam environments. Washington, DC: U.S. Nuclear Regulatory Commission, 1997.

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17

Ahuja, J. K. Investigation of hypersonic shock-induced combustion in a hydrogen-air system. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.

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18

N, Tiwari S., Singh D. J e 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.

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19

N, Tiwari S., e 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.

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20

N, Tiwari S., e 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.

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21

Skyring, R. Experimental determination of hydrogen-air detonation pressure limit and scramjet application. Washington: American Institute of Aeronautics and Astronautics, 1996.

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22

Thorne, 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.

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23

Domel, 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.

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24

United 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.

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25

Hitch, B. D. Reduced H2-O2 mechanisms for use in reacting flow simulation. New York: AIAA, 1988.

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26

J, Breisacher Kevin, e United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.

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27

J, Breisacher Kevin, e United States. National Aeronautics and Space Administration., eds. A comparison of analytical results for 20 K LOX/hydrogen instabilities. [Washington, D.C.]: NASA, 1990.

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28

Rumminger, 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.

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29

Wong, 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.

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30

L, Olson Sandra, e 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.

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31

L, Olson Sandra, e 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.

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32

N, Tiwari S., e 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.

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33

N, Tiwari S., e 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.

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34

Huang, Morren Sybil, e 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.

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35

R, Tieszen S., Benedick William B, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Systems Research. e 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.

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36

Kanilo, P. M. Ėnergeticheskie i ėkologicheskie kharakteristiki GTD pri ispolʹzovanii uglevodorodnykh topliv i vodoroda. Kiev: Nauk. dumka, 1987.

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37

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) e 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.

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38

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) e 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.

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39

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) e 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.

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40

R, Thomas S., e 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.

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41

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) e 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.

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42

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) e 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.

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43

Rosa, 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.

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44

Rosa, 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.

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45

U.S. Nuclear Regulatory Commission. Office of Nuclear Reactor Regulation. Division of Engineering and System Technology. e 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.

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46

J, Schneider Steven, e 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.

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47

J, Schneider Steven, e 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.

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48

M, Kazaroff John, Jankovsky Robert S e 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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49

M, Kazaroff John, Jankovsky Robert S e 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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50

M, Kazaroff John, Jankovsky Robert S e 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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