Libros sobre el tema "Combustore"

Young, Mark F. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1988.

Lee, Richard S. L., James H. Whitelaw y T. S. Wung, eds. Aerothermodynamics in Combustors. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-84755-4.

Center, Langley Research, ed. HYPULSE combustor analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Center, Langley Research, ed. HYPULSE combustor analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Lieuwen, Timothy C. Unsteady combustor physics. Cambridge: Cambridge University Press, 2013.

Kumar, Sanjiv. A computer model for the simulation of turbulent reacting flow in a jet assisted ram combustor. Chofu, Tokyo: National Aerospace Laboratory, 1995.

M, Mellor A., ed. Design of modern turbine combustors. London: Academic Press, 1990.

United States. Environmental Protection Agency. Office of Water, ed. Development document for final effluent limitations guidelines and standards for the commercial hazardous waste combustor subcategory of the waste combustors point source category. Washington, DC: U.S. Environmental Protection Agency, Office of Water, 2000.

J, Breisacher Kevin y United States. National Aeronautics and Space Administration., eds. 3D rocket combustor acoustics model. [Washington, DC]: National Aeronautics and Space Administration, 1992.

P, Menees Gene y Ames Research Center, eds. Wave combustors for trans-atmospheric vehicles. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

Construction Engineering Research Laboratories (U.S.), ed. Environmental considerations for municipal waste combustors. [Champaign, IL]: US Army Corps of Engineers, Construction Engineering Research Laboratories, 1994.

Drummond, J. Philip. Mixing enhancement in a supersonic combustor. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.

Melconian, Jerry O. Introducing the VRT gas turbine combustor. [Washington, D.C.]: NASA, 1990.

Hernandez, Maria Barrio. Modelling of a fluidized bed combustor. Manchester: UMIST, 1995.

Unit, Energy Technology Support. High capacity whole-bale straw combustor. London: Department of Trade and Industry, 1994.

Gordon, Sanford. Finite area combustor theoretical rocket performance. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Lyczkowski, Robert W., Walter F. Podolski, Jacques X. Bouillard y Stephen M. Folga. Thermo-Hydrodynamic Design of Fluidized Bed Combustors. New York, NY: Springer New York, 2012. http://dx.doi.org/10.1007/978-1-4614-3591-4.

1957-, Gullett Brian Kent, Jozewicz Wojciech y United States. Environmental Protection Agency, eds. Control of mercury emissions from coal combustors. [Washington, D.C.?: U.S. Environmental Protection Agency, 1996.

Fuller, E. J. Integrated CFD modeling of gas turbine combustors. Washington, D. C: AIAA, 1993.

Jacobs, P. A. Preliminary calibration of a generic scramjet combustor. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1991.

David, Jiri. Emissions from a gas-burning pulse combustor. London: Middlesex University, 1993.

United States. National Aeronautics and Space Administration., ed. Composite matrix experimental combustor: Final technical report. [Washington, D.C.]: NASA, 1994.

United States. National Aeronautics and Space Administration., ed. LDV measurements in an annular combustor model. West Lafayette, Ind: Purdue University, School of Aeronautics and Astronautics, 1989.

United States. National Aeronautics and Space Administration., ed. LDV measurements in an annular combustor model. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Jacobs, P. A. Flow establishment in a generic scramjet combustor. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

A, Jacobs Peter y Langley Research Center, eds. Flow establishment in a generic scramjet combustor. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. High-temperature durability considerations for HSCT combustor. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

F, Sens P., Wilkinson J. K y Commission of the European Communities. Directorate-General for Science, Research, and Development., eds. Fluidized bed combustor design, construction, and operation. London: Elsevier Applied Science, 1988.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. High-temperature durability considerations for HSCT combustor. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

A, Jacobs Peter y Langley Research Center, eds. Preliminary calibration of a generic scramjet combustor. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, [1991], 1991.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. High-temperature durability considerations for HSCT combustor. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Jacobson, Nathan S. High-temperature durability considerations for HSCT combustor. Cleveland, Ohio: Lewis Research Center, 1992.

United States. National Aeronautics and Space Administration., ed. Energy efficient engine: Combustor component performance progam. [Washington, DC: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.

Simone, L. De. La combustione in letto fluido. Roma: ENEA, Comitato nazionale per la ricerca e per lo sviluppo dell'energia nucleare e delle energie alternative, 1987.

Simone, L. De. La combustione in letto fluido. Roma: ENEA, Comitato nazionale per la ricerca e per lo sviluppo dell'energia nucleare e delle energie alternative, 1987.

Bennett, J. S. Gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1986.

Janicka, Johannes, Amsini Sadiki, Michael Schäfer y Christof Heeger, eds. Flow and Combustion in Advanced Gas Turbine Combustors. Dordrecht: Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5320-4.

Lee, R. S. L. Aerothermodynamics in Combustors: IUTAM Symposium Taipei, Taiwan, 1991. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992.

Menon, S. Shock-wave-induced mixing enhancement in scramjet combustors. Washington, D. C: American Institute of Aeronautics and Astronautics, 1989.

Janicka, Johannes. Flow and Combustion in Advanced Gas Turbine Combustors. Dordrecht: Springer Netherlands, 2013.

Libbis, N. Coal particle behaviour in a counter-current combustor. Haifa: Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1987.

United States. Environmental Protection Agency. Office of Air Quality Planning and Standards, ed. Municipal waste combustor operator training program: Course manual. Research Triangle, N.C: U.S. Environmental Protection Agency, Office of Air Quality Planning and Standards, 1993.

Krishna, Kundu, Ghorashi Bahman y United States. National Aeronautics and Space Administration., eds. Simplified Jet-A kinetic mechanism for combustor application. [Washington, DC: National Aeronautics and Space Administration, 1993.

Sattar, M. A. Advanced composite combustor structural concepts program: Final report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

P, Kundu Krishna, Ghorashi Bahman y United States. National Aeronautics and Space Administration., eds. Simplified Jet-A kinetic mechanism for combustor application. [Washington, DC: National Aeronautics and Space Administration, 1993.

Reid, Smith y Lewis Research Center, eds. Advanced low emissions subsonic combustor study: Final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Investigations of flowfields found in typical combustor geometries. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

P, Kundu Krishna, Ghorashi Bahman y United States. National Aeronautics and Space Administration., eds. Simplified Jet-A kinetic mechanism for combustor application. [Washington, DC: National Aeronautics and Space Administration, 1993.