The Online Books Page

Gas-turbines -- Combustion chambers -- Research

See also what's at your library, or elsewhere.

• Gas-turbines -- Combustion chambers
• Gas-turbines -- Research

• Gas-turbines -- Combustion chambers -- Research -- California

• Energy Innovations Small Grant Program, Environmentally-preferred Advanced Generation (California Energy Commission, 2001), by John D Sullivan, Hal Clark, Alzeta Corporation, Energy Innovations Small Grant Program, and California Energy Commission. Public Interest Energy Research (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Effect of primary-zone equivalence ratio and hydrogen addition on exhaust emission in a hydrocarbon-fueled combustor (National Aeronautics and Space Administration ;, 1974), by Carl T. Norgren, Robert D. Ingebo, and Lewis Research Center (page images at HathiTrust)
• Scanning radiometer for measurement of forward-scattered light to determine mean diameter of spray particles (National Aeronautics and Space Administration ;, 1976), by Donald R. Buchele and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of flameholder pressure drop on emissions and performance of premixed-prevaporized combustors (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Robert A. Duerr, Valerie J. Lyons, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Film cooling in a combustor operating at fuel-rich exit conditions (National Aeronautics and Space Administration ;, 1974), by Robert R. Tacina, Cecil J. Marek, and Lewis Research Center (page images at HathiTrust)
• Threshold fatigue crack growth behavior (Wright-Patterson Air Force Base, Ohio : Materials Laboratory, Wright Research Development Center, Air Force Systems Command, United States Air Force, XXXX, 1989), by F. K. Haake, Clifford G. Annis, J. W. Fischer, Gary Charles Salivar, E. H. Hindle, Wright Research Development Center, Pratt & Whitney Aircraft Group. Government Products Division, and United States. Air Force. Systems Command (page images at HathiTrust)

• Analysis of total-pressure loss and airflow distribution for annular gas turbine combustors (National Aeronautics and Space Administration ;, 1969), by Robert R. Tacina, Jack Grobman, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)

• Effect of free-stream turbulence on film cooling (National Aeronautics and Space Administration ;, 1975), by Cecil J. Marek, Robert R. Tacina, and Lewis Research Center (page images at HathiTrust)
• Film cooling in a combustor operating at fuel-rich exit conditions (National Aeronautics and Space Administration ;, 1974), by Robert R. Tacina, Cecil J. Marek, and Lewis Research Center (page images at HathiTrust)

• Measurements of liner cooling effectiveness within a full-scale double-annular ram-induction combustor (National Aeronautics and Space Administration ;, 1974), by Edward J. Mularz, Donald F. Schultz, and U.S. Army Air Mobility Research and Development Laboratory (page images at HathiTrust)

• Energy Innovations Small Grant Program, Environmentally-preferred Advanced Generation (California Energy Commission, 2001), by John D Sullivan, Hal Clark, Alzeta Corporation, Energy Innovations Small Grant Program, and California Energy Commission. Public Interest Energy Research (page images at HathiTrust)

• Effect of design features on performance of a double-annular ram-induction combustor (National Aeronautics and Space Administration ;, 1975), by Donald F. Schultz and Lewis Research Center (page images at HathiTrust)

• Energy Innovations Small Grant Program, Environmentally-preferred Advanced Generation (California Energy Commission, 2001), by John D Sullivan, Hal Clark, Alzeta Corporation, Energy Innovations Small Grant Program, and California Energy Commission. Public Interest Energy Research (page images at HathiTrust)

• Performance of a vortex-controlled diffuser in an annular swirl-can combustor at inlet Mach numbers up to 0.53 (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979), by John M. Smith (page images at HathiTrust)
• Effect of fuel injector type on performance and emissions of reverse-flow combustor (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981), by Carl T. Norgren and Stephen M. Riddlebaugh (page images at HathiTrust)
• Performance and emission characteristics of swirl-can combustors to a near-stoichiometric fuel-air ratio (National Aeronautics and Space Administration :, 1976), by Larry A. Diehl, Arthur M. Trout, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of inlet-air humidity, temperature, pressure, and reference Mach number on the formation of oxides of nitrogen in a gas turbine combustor (National Aeronautics and Space Administration ;, 1973), by Nicholas R. Marchionna, Arthur M. Trout, Larry A. Diehl, and Lewis Research Center (page images at HathiTrust)

• Effect of diffuser bleed on performance of an annular swirl can combustor (National Aeronautics and Space Administration ;, 1974), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• Modifications that improve performance of a double annular combustor at simulated engine idle conditions (National Aeronautics and Space Administration ;, 1974), by Donald F. Schultz and Lewis Research Center (page images at HathiTrust)
• Variable combustor geometry for improving the altitude relight capability of a double annular combustor (National Aeronautics and Space Administration ;, 1974), by Donald F. Schultz and Lewis Research Center (page images at HathiTrust)
• Exhaust emissions of a double annular combustor : parametric study (National Aeronautics and Space Administration ;, 1975), by Donald F. Schultz and Lewis Research Center (page images at HathiTrust)
• Idle efficiency and pollution results for two-row swirl-can combustors having 72 modules (National Aeronautics and Space Administration ;, 1975), by James A. Biaglow, Arthur M. Trout, and Lewis Research Center (page images at HathiTrust)
• Ground idle performance improvement of a double-annular combustor by using simulated variable combustor geometry (National Aeronautics and Space Administration ;, 1975), by Donald F. Schultz and Lewis Research Center (page images at HathiTrust)
• Performance of a short modular turbojet combustor segment using ASTM-A1 fuel (National Aeronautics and Space Administration ;, 1971), by Richard W. Niedzwiecki, Harry M. Moyer, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Combustion stability of single swirl-can combustor modules using ASTM-A1 liquid fuel (National Aeronautics and Space Administration ;, 1969), by Richard W. Niedzwiecki, Robert E. Jones, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Performance of a 48-module swirl-can turbojet combustor segment at high temperatures using ASTM-A1 fuel (National Aeronautics and Space Administration ;, 1969), by Richard W. Niedzwiecki, Harry M. Moyer, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-6706 (National Aeronautics and Space Administration :, 1972), by Donald F. Schultz, Porter J. Perkins, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Effect of flame stabilizer design on performance and exhaust pollutants of a two-row swirl-can combustor operated to near-stoichiometric conditions (National Aeronautics and Space Administration ;, 1977), by James A. Biaglow, Arthur M. Trout, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Emissions of nitrogen oxides from an experimental hydrogen-fueled gas turbine combustor (National Aeronautics and Space Administration ;, 1974), by Carl T. Norgren, Robert D. Ingebo, and Lewis Research Center (page images at HathiTrust)
• Optical measurement of static temperature and hydroxyl radical profiles in a hydrogen-fueled supersonic combustor (National Aeronautics and Space Administration ;, 1974), by Raymond E. Gaugler and Lewis Research Center (page images at HathiTrust)
• Spontaneous-ignition temperature limits of Jet A fuel in research-combustor segment (National Aeronautics and Space Administration ;, 1974), by Robert D. Ingebo, Carl T. Norgren, and Lewis Research Center (page images at HathiTrust)
• Effect of oxygen addition on altitude blowout and relight of an experimental combustor segment (National Aeronautics and Space Administration ;, 1974), by Carl T. Norgren, Robert D. Ingebo, and Lewis Research Center (page images at HathiTrust)
• Performance and durability of improved air-atomizing splash-cone fuel nozzles (National Aeronautics and Space Administration ;, 1974), by Robert D. Ingebo, Carl T. Norgren, and Lewis Research Center (page images at HathiTrust)
• Effect of exhaust gas recirculation on emissions from a flame-tube combustor using liquid Jet A Fuel (National Aeronautics and Space Administration ;, 1976), by Cecil J. Marek, Robert R. Tacina, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Exhaust pollutant emissions from swirl-can combustor module arrays at parametric test conditions (National Aeronautics and Space Administration ;, 1975), by Edward J. Mularz, Peter W. Verbulecz, Jerrold D. Wear, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• Flow characteristics of various swirl-can module designs (National Aeronautics and Space Administration ;, 1975), by Edward J. Mularz, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• Effect of wall edge suction on the performance of a short annular dump diffuser with exit passage flow resistance (National Aeronautics and Space Administration ;, 1975), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• Effect of premixing quality on oxides of nitrogen in gas turbine combustors (National Aeronautics and Space Administration ;, 1976), by Gerald Roffe, Antonio Ferri, Lewis Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Prevaporization and premixing to obtain low oxides of nitrogen in gas turbine combustors (National Aeronautics and Space Administration ;, 1975), by Gerald Roffe, Antonio Ferri, Lewis Research Center, and Advanced Technology Laboratories (page images at HathiTrust)
• Investigation of hydrogen-air ignition senitized by nitric oxide and by nitrogen dioxide (National Aeronautics and Space Administration ;, 1977), by M. Slack, A. Grillo, Grumman Aerospace Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Pollutant formation in fuel lean reciruclating flows (National Aeronautics and Space Administration ;, 1976), by Robert W. Schefer, R. F. Sawyer, Berkeley University of California, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of design features on performance of a double-annular ram-induction combustor (National Aeronautics and Space Administration ;, 1975), by Donald F. Schultz and Lewis Research Center (page images at HathiTrust)
• Performance of an asymmetric short annular diffuser with a nondiverging inner wall using suction (National Aeronautics and Space Administration ;, 1974), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• Aerodynamic drag and fuel spreading measurements in a simulated scramjet combustion module (National Aeronautics and Space Administration ;, 1974), by Louis A. Povinelli and Lewis Research Center (page images at HathiTrust)

• Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth (NACA, 1954), by William K. Koffel, United States National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)

• NASA TN D-6297 (National Aeronautics and Space Administration:, 1971), by Frank W. Burcham (page images at HathiTrust; US access only)
• Supersonic inlet investigation. Volume I, Summary report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by T. W. Tsukahira, Gordon R. Hall, M. Yaamada, W. F. Wong, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Supersonic inlet investigation. Volume III, Wind tunnel data report (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by T. W. Tsukahira, B. G. Franco, W. F. Wong, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)
• Supersonic inlet investigation. Volume II, Air induction sysem dynamic simulation model (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by Nasim F. Amin, Gordon R. Hall, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Northrop Corporation. Aircraft Division (page images at HathiTrust)

• Energy Innovations Small Grant Program : Environmentally-preferred Advanced Generation (California Energy Commission, 2003), by Ḥasan Karīm, Shahrokh Etemad, Hal Clark, Energy Innovations Small Grant Program, California Energy Commission. Public Interest Energy Research, Precision Combustion Inc, and San Diego State University. Foundation (page images at HathiTrust)

• High efficiency gas turbines : report (to accompany H.R. 3029) (including cost estimate of the Congressional Budget Office). (U.S. G.P.O., 2009), by United States. Congress. House. Committee on Science and Technology (2007) (page images at HathiTrust)

More items available under broader and related terms at left.