Books on the topic 'Gas turbine fuels'

Lefebvre, Arthur H. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.

R, Ballal Dilip, ed. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.

Odgers, J. Gas turbine fuels and their influence on combustion. Turnbridge Wells, Kent: Abacus Press, 1986.

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

Gardner, L. Alternative transportation fuels: review of research activity in Canada: Report of the Task Force on Alternative Fuels, Associate Committee on Propulsion, National Research Council Canada = Combustibles de transport de remplacement: examen des travaux de recherche au Canada : rapport du Groupe de travail sur les combustibles de remplacement : Comite associe sur la propulsion, Conseil national de recherches du Canada. Ottawa: National Research Council Canada, Division of Mechanical Engineering, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Symposium. Combustion and fuels in gas turbine engines: Papers presented at the Propulsion and Energetics Panel 70th Symposium held in Chania, Crete, Greece, on 19-23 October 1987. Neuilly-sur-Seine, France: Advisory Group for Aerospace Research & Development, 1988.

Cawley, James D. Phenomenological study of the behavior of some silica formers in a high velocity jet fuel burner. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

Colket, Meredith, and Joshua Heyne, eds. Fuel Effects on Operability of Aircraft Gas Turbine Combustors. Reston, VA: American Institute of Aeronautics and Astronautics, Inc., 2021. http://dx.doi.org/10.2514/4.106040.

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

Gorla, Rama S. R. Probabilistic analysis of solid oxide fuel cell based hybrid gas turbine system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

Aerospace Technology Conference & Exposition (1985 Long Beach, Calif.). Aviation gas turbine lubricants: Military and civil aspects ; Aviation fuel and lubricants : performance testing. Warrendale, PA: Society of Automotive Engineers, 1985.

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

Research and Technology Organization. Applied Vehicle Technology Panel. Symposium. Gas turbine engine combustion, emissions and alternative fuels =: La combustion dans les turbomoteurs, les emissions et les carburants de remplacement : papers presented at the Applied Vehicle Technology Panel Symposium organised by the former AGARD Propulsion and Energetics Panel held in Lisbon, Portugal, 12-16 October 1998. Neuilly-sur-Seine: Research and Technology Organization, 1999.

Tacina, Robert R. Flame tube NOx emissions using a lean-direct-wall-injection combustor concept. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Kyōkai, Enjiniaringu Shinkō. Shin sūpā gomi hatsuden to kison (matawa shinki) infura katsuyō ni yoru PFI jigyōka chōsa: Hōkokusho : Heisei 16-nendo minkan shikin katsuyō tō keizai seisaku suishin. Tōkyō: Enjiniaringu Shinkō Kyōkai, 2005.

Lattime, Scott B. Turbine engine clearance control systems: Current practices and future directions. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Douwe, Stapersma, ed. Design of propulsion and electric power generation systems. London: IMarEST, Institute of Marine Engineering, Science and Technology, 2002.

John, D. St. Effect of jet injection angle and number of jets on mixing and emissions from a reacting crossflow at atmospheric pressure. [Washington, D.C.]: National Aeronautics and Space Administration STI Preogram Office, 2000.

Woud, Hans Klein. Design of propulsion and electric power generation systems. London: IMarEST, Institute of Marine Engineering, Science and Technology, 2002.

Woud, Hans Klein. Design of propulsion and electric power generation systems. London: IMarEST, Institute of Marine Engineering, Science and Technology, 2002.

Bunk, W. Evaluation of COST project 50 'Materials for gas turbines' and COST project 501 'High temperature materials for conventional systems of energy generation and conversion using fossil fuels'. Luxembourg: Commission of the European Communities, 1985.

International Joint Power Generation Conference (2000 Miami Beach, Fla.). Proceedings of the 2000 International Joint Power Generation Conference: Power, fuels and combustion technologies, nuclear engineering : presented at the 2000 International Joint Power Generation Conference, July 23-26, 2000, Miami Beach, Florida. New York, N.Y: American Society of Mechanical Engineers, 2000.

International Joint Power Generation Conference (2001 New Orleans, Louisiana). Proceedings of the 2001 International Joint Power Generation Conference: Presented at the 2001 International Joint Power Generation Conference : June 4-7, 2001, New Orleans, Louisiana. New York: American Society of Mechanical Engineers, 2001.

International Joint Power Generation Conference (2002 Scottsdale, Ariz.). Proceedings of the IJPGC 2002 International Joint Power Generation Conference: Presented at the 2002 International Joint Power Generation Conference : June 24-26, 2002, Scottsdale, Arizona. New York, N.Y: American Society of Mechanical Engineers, 2002.

International Joint Power Generation Conference (2003 Atlanta, Ga.). Proceedings of the 2003 International Joint Power Generation Conference: Presented at the 2003 International Joint Power Generation Conference : June 16-19, 2003, Atlanta, Georgia. New York, N.Y: American Society of Mechanical Engineers, 2003.

United States. Dept. of Energy. Office of Transportation Systems. and United States. National Aeronautics and Space Administration., eds. Gas turbine alternative fuels combustion characteristics. Washington, D.C: U.S. Dept. of Energy, Conservation and Renewable Energy, Office of Transportation Systems, 1989.

United States. National Aeronautics and Space Administration., ed. Combustion characteristics of gas turbine alternative fuels. [Washington, DC: National Aeronautics and Space Administration, 1987.

Rez, Peter. Electrical Power Generation: Fossil Fuels. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780198802297.003.0004.

Lefebvre, Arthur H., and Dilip R. Ballal. Gas Turbine Combustion: Alternative Fuels and Emissions, Third Edition. Taylor & Francis Group, 2010.

Hoppesteyn, Peter Dirk Jilles. Application of Low Calorific Value Gaseous Fuels in Gas Turbine Combustors. Delft Univ Pr, 1999.

Odgers, A. K. Gas Turbine Fuels and Their Influence on Combustion (Energy and Engineering Science Series). Taylor & Francis, 1986.

United States. National Aeronautics and Space Administration., ed. ATTAP Advanced Turbine Technology Applications Project: 1991 annual report. Indianapolis, Ind: Allison, Gas Turbine Division, General Motors Corporation, 1992.

Organization, North Atlantic Treaty. Combustion and fuels in gas turbine engines: Papers presented at the Propulsion and Energetics Panel 70th Symposium held in Chania, Crete, Greece, on 19-23 October 1987 (AGARD conference proceedings). Advisory Group for Aerospace Research & Development, 1988.

United States. National Aeronautics and Space Administration., ed. Component testing of a ground based gas turbine steam cooled rich-burn primary zone combustor for emissions control of nitrogenous fuels. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

United States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

Wave rotor-enhanced gas turbine engines. [Washington, DC]: National Aeronautics and Space Administration, 1995.

M, Jones Scott, Paxson Daniel E, and United States. National Aeronautics and Space Administration., eds. Wave rotor-enhanced gas turbine engines. [Washington, DC]: National Aeronautics and Space Administration, 1995.

M, Jones Scott, Paxson Daniel E, and United States. National Aeronautics and Space Administration., eds. Wave rotor-enhanced gas turbine engines. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Wolf, E. L. Physics and Technology of Sustainable Energy. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198769804.001.0001.

Asme Turbo Expo: Biomass and Alternative Fuels, Innovations. American Society of Mechanical Engineers, 2004.

United States. National Aeronautics and Space Administration., ed. Automotive gas turbine power system-performance analysis code. [Washington, DC]: National Aeronautics and Space Administration, 1997.

James, Rollbuhler R., Lezberg Erwin A, and United States. National Aeronautics and Space Administration., eds. Fuel-rich catalytic combustion: A fuel processor for high-speed propulsion. [Washington, D.C.]: NASA, 1990.

James, Rollbuhler R., Lezberg Erwin A, and United States. National Aeronautics and Space Administration., eds. Fuel-rich catalytic combustion: A fuel processor for high-speed propulsion. [Washington, D.C.]: NASA, 1990.

Fuel-rich catalytic combustion: A fuel processor for high-speed propulsion. [Washington, D.C.]: NASA, 1990.

Fuel rich catalytic combustion, the first stage of a two-stage combustor. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

Hnydiuk-Stefan, Anna. Dual-Fuel Gas-Steam Power Block Analysis: Methodology and Continuous-Time Mathematical Models. Springer, 2018.