Książki na temat „Premixed Combustion”

Turbulent premixed flames. Cambridge: Cambridge University Press, 2011.

Santavicca, D. A. Premixed turbulent flame propagation. University Park, PA: Pennsylvania State University, 1987.

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

Chinitz, Wallace. Experimental requirements for the study of shock-induced premixed combustion. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.

V, Bracco Frediano, red. Two-dimensional visualization of premixed-charge flame structure in an IC engine. Warrendale, PA: Society of Automotive Engineers, 1987.

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.

Mantzaras, John. Three-dimensional visualization of premixed-charge engine flames: Islands of reactants and products, fractal dimensions, and homogeneity. Warrendale, PA: Society of Automotive Engineers, 1988.

Xie, Lin. Effects of jet strength on NOx formation in premixed impinging jet combustion with minimum heat losses. Tokyo, Japan: National Aerospace Laboratory, 1994.

Nguyen, Hung Lee. Evaluation of a hybrid kinetics/mixing-controlled combustion model for turbulent premixed and diffusion combustion using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1990.

Herrmann, Marcus. Numerical simulation of premixed turbulent combustion based on a level set flamelet model. Aachen: Shaker, 2001.

Nikjooy, Mohammad. On the modelling of non-reactive and reactive turbulent combustor flows. Cleveland, Ohio: Lewis Research Center, 1987.

Paxson, Daniel E. A sectored-one-dimensional model for simulating combustion instabilities in premix combustors. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Paxson, Daniel E. A sectored-one-dimensional model for simulating combustion instabilities in premix combustors. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Paxson, Daniel E. A sectored-one-dimensional model for simulating combustion instabilities in premix combustors. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Singh, D. J. Numerical simulation of shock-induced combustion/detonation in a premixed H2-air mixture using Navier-Stokes equations. Washington, D. C: American Institute of Aeronautics and Astronautics, 1991.

Bray, K. N. C., i Nedunchezhian Swaminathan. Turbulent Premixed Flames. University of Cambridge ESOL Examinations, 2014.

Lipatnikov, Andrei. Fundamentals of Premixed Turbulent Combustion. Taylor & Francis Group, 2012.

Fundamentals Of Premixed Turbulent Combustion. Taylor & Francis Inc, 2012.

Lipatnikov, Andrei. Fundamentals of Premixed Turbulent Combustion. Taylor & Francis Group, 2017.

Lipatnikov, Andrei. Fundamentals of Premixed Turbulent Combustion. CRC Press, 2012. http://dx.doi.org/10.1201/b12973.

Krishnan, Radhakrishnan, Oyediran Ayo i United States. National Aeronautics and Space Administration., red. Combustion noise at elevated pressures in a liquid-fueled premixed combustor. [Washington, DC]: National Aeronautics and Space Administration, 1997.

L, Berlad A., i United States. National Aeronautics and Space Administration., red. The structure of particle cloud premixed flames. [Washington, DC: National Aeronautics and Space Administration, 1993.

Hossain, Mamdud. CFD modelling of turbulent non-premixed combustion. 1999.

Benim, Ali Cemal, i Khawar Jamil Syed. Flashback Mechanisms in Lean Premixed Gas Turbine Combustion. Elsevier Science & Technology Books, 2014.

Flashback Mechanisms in Lean Premixed Gas Turbine Combustion. Elsevier, 2015. http://dx.doi.org/10.1016/c2013-0-18847-2.

United States. National Aeronautics and Space Administration., red. Numerical prediction of turbulent flame stability in premixed/prevaporized (HSCT) combustors. [Washington, DC: National Aeronautics and Space Administration, 1990.

Combustion-acoustic stability analysis for premixed gas turbine combustors. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Combustion-acoustic stability analysis for premixed gas turbine combustors. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

M, Deur J., i United States. National Aeronautics and Space Administration., red. Analysis of lean premixed/prevaporized combustion with KIVA-II. [Washington, D.C: National Aeronautics and Space Administration, 1994.

Douglas, Darling, i United States. National Aeronautics and Space Administration., red. Combustion-acoustic stability analysis for premixed gas turbine combustors. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Douglas, Darling, i United States. National Aeronautics and Space Administration., red. Combustion-acoustic stability analysis for premixed gas turbine combustors. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

G, Patnaik, Oran Elaine S i United States. National Aeronautics and Space Administration., red. Time-dependent computational studies of premixed flames in microgravity. [Washington, DC]: National Aeronautics and Space Administration, 1993.

G, Patnaik, Oran Elaine S i United States. National Aeronautics and Space Administration., red. Time-dependent computational studies of premixed flames in microgravity. [Washington, DC]: National Aeronautics and Space Administration, 1993.

G, Patnaik, Oran Elaine S i United States. National Aeronautics and Space Administration., red. Time-dependent computational studies of premixed flames in microgravity. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Sensitivity of combustion-acoustic instabilities to boundary conditions for premixed gas turbinecombustors. [Washington, DC]: National Aeronautics and Space Administration, 1995.

On the modelling of non-reactive and reactive turbulent combustor flows. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

C, So Ronald M., i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., red. On the modelling of non-reactive and reactive turbulent combustor flows. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Center, NASA Glenn Research, red. A sectored-one-dimensional model for simulating combustion instabilities in premix combustors. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 1999.

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) i Building and Fire Research Laboratory (U.S.), red. 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.

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) i Building and Fire Research Laboratory (U.S.), red. 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.

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) i Building and Fire Research Laboratory (U.S.), red. 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.

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.

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) i Building and Fire Research Laboratory (U.S.), red. 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.

D, Rumminger Marc, Babushok Valeri, National Institute of Standards and Technology (U.S.) i Building and Fire Research Laboratory (U.S.), red. 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.

Flamelet model application for non-premixed turbulent combustion: Final report under cooperative agreement no. NCCW-75 ... Moscow, [Russia]: Ecolen Scientific Research Center, 1996.

A, Strehlow Roger, University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Dept i United States. National Aeronautics and Space Administration, red. The behavior of fuel-lean premixed flames in a standard flammability limit tube under controlled gravity conditions. Urbana, Ill: Aeronautical and Astronautical Engineering Dept., University of Illinois, 1986.

The behavior of fuel-lean premixed flames in a standard flammability limit tube under controlled gravity conditions. Urbana, Ill: Aeronautical and Astronautical Engineering Dept., University of Illinois, 1986.

A, Strehlow Roger, University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Dept. i United States. National Aeronautics and Space Administration., red. The behavior of fuel-lean premixed flames in a standard flammability limit tube under controlled gravity conditions. Urbana, Ill: Aeronautical and Astronautical Engineering Dept., University of Illinois, 1986.

A, Strehlow Roger, University of Illinois at Urbana-Champaign. Aeronautical and Astronautical Engineering Dept i United States. National Aeronautics and Space Administration, red. The behavior of fuel-lean premixed flames in a standard flammability limit tube under controlled gravity conditions. Urbana, Ill: Aeronautical and Astronautical Engineering Dept., University of Illinois, 1986.

Center, Lewis Research, red. Improved modeling of finite-rate turbulent combustion processes in research combustors. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.