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Combustion chambers -- Testing

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• Combustion chambers
• Internal combustion engines -- Testing
• Testing

• Aircraft gas-turbines -- Combustion chambers -- Testing
• Airplanes -- Turbojet engines -- Combustion chambers -- Testing
• Combustion chambers -- Materials -- Testing
• Gas-turbines -- Combustion chambers -- Testing

• Effect of primary-zone water injection on pollutants from a combustor burning liquid ASTM A-1 and vaporized propane fuels (National Aeronautics and Space Administration ;, 1973), by Robert D. Ingebo, Carl T. Norgren, and Lewis Research Center (page images at HathiTrust)
• Relation of emitted ultraviolet radiation to combustion of hydrogen and oxygen at 20 atmospheres (National Aeronautics and Space Administration :, 1964), by Marshall C. Burrows, Ronald Razner, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-6435 (National Aeronautics and Space Administration ;, 1971), by Albert J. Juhasz, J. D. Holdeman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Radiation processes related to oxygen-hydrogen combustion at high pressures (National Aeronautics and Space Administration :, 1964), by Marshall C. Burrows and Lewis Research Center (page images at HathiTrust)
• High-pressure combustor exhaust emissions with improved air-atomizing and conventional pressure-atomizing fuel nozzles (National Aeronautics and Space Administration ;, 1973), by Robert D. Ingebo, Carl T. Norgren, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Experiments with hydrogen and oxygen in regenerative engines at chamber pressures from 100 to 300 pounds per square inch absolute (National Aeronautics and Space Administration, 1960), by William A. Tomazic, R. James Rollbuhler, Edward R. Bartoo, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-7021 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Donald F. Schultz, Jerrold D. Wear, Porter J. Perkins, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Afterburner performance of circular v-gutters and a sector of parallel v-gutters for a range of inlet temperatures to 1255 K (1800 ̊F) (National Aeronautics and Space Administration ;, 1973), by J. Robert Branstetter, Gregory M. Reck, and Lewis Research Center (page images at HathiTrust)
• Seven commercial organo-metallic additives (National Advisory Committee for Aeronautics, 1954), by Vincent F. Hlavin, William P. Cook, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Effect of fuel additives on carbon deposition in a J33 single combustor [Part] 1, Three metallic-organic additives (National Advisory Committee for Aeronautics, 1952), by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), by Bemrose Boyd, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Sonotech, Inc. frequency-tunable pulse combustion system (Cello Pulse Burner) : innovative technology evaluation report. (National Risk Management Research Laboratory, 1997), by National Risk Management Research Laboratory (U.S.), United States. Environmental Protection Agency. Office of Research and Development, and Inc Sonotech (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)

• Performance of short length turbojet combustor insensitive to radial distortion of inlet airflow (National Aeronautics and Space Administration ;, 1970), by Francis M. Humenik, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)

• Conventionally cast and forged copper alloy for high-heat-flux thrust chambers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by John M. Kazaroff, George A. Repas, and Lewis Research Center (page images at HathiTrust)

• Reliability and effective thermal conductivity of three metallic-ceramic composite insulating coatings on cooled hydrogen-oxygen rockets (National Aeronautics and Space Administration ;, 1973), by Harold G. Price, Richard J. Quentmeyer, Ralph L. Schacht, and Lewis Research Center (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)

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

• Evaluation of a thin-film, heat-flux probe for measuring gas velocities in an unstable rocket combustor (National Aeronautics and Space Administration ;, 1967), by Frederick P. Povinelli, Robert D. Ingebo, and Lewis Research Center (page images at HathiTrust)
• Drag and distribution measurements of single-element fuel injectors for supersonic combustors (National Aeronautics and Space Administration ;, 1974), by Louis A. Povinelli and Lewis Research Center (page images at HathiTrust)
• Effect of hydrogen injection stability and emissions of an experimental premixed prevaporized propane burner (National Aeronautics and Space Administration ;, 1975), by David N. Anderson and Lewis Research Center (page images at HathiTrust)
• Effect of wall suction on performance of a short annular diffuser at inlet Mach numbers up to 0.5 (National Aeronautics and Space Administration ;, 1975), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• Development of a barium chemical release system (National Aeronautics and Space Administration ;, 1969), by C. S. Stokes, W. J. Murphy, E. W. Smith, Temple University, and Langley Research Center (page images at HathiTrust)
• NASA TN D-3729 (National Aeronautics and Space Administration [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1966), by Curtis R. Bailey, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Nonreactive mixing study of a scramjet swept-strut fuel injector (National Aeronautics and Space Administration ;, 1975), by Charles R. McClinton and Langley Research Center (page images at HathiTrust)
• NASA TN D-5688 (National Aeronautics and Space Administration ;, 1970), by Richard W. Niedzwiecki, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental determination of the temperature and dynamic-strain environment of a tubular combustor liner in a turbojet engine (National Aeronautics and Space Administration, 1960), by Patrick T. Chiarito, C. Robert Morse, William C. Morgan, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-5733 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Nicholas R. Marchionna, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Magnetic control of the flow of hot combustion gases in hydrogen-oxygen combustion at 14 atmospheres (National Aeronautics and Space Administration ;, 1965), by Ronald Razner and Lewis Research Center (page images at HathiTrust)
• NASA TN D-6410 (National Aeronautics and Space Administration ;, 1971), by Carl T. Norgren, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gaseous-hydrogen, liquid-oxygen rocket combustion at supercritical chamber pressures (National Aeronautics and Space Administration ;, 1967), by Martin Hersch, Edward J. Rice, and Lewis Research Center (page images at HathiTrust)
• Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions (National Aeronautics and Space Administration ;, 1969), by Helmut F. Butze, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Vaporization rates of ethanol sprays in a combustor with low-frequency fluctuations of combustion-gas pressure / Robert D. Ingebo. (National Aeronautics and Space Administration :, 1962), by Robert D. Ingebo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of a hydrogen burner to simulate air entering scramjet combustors (National Aeronautics and Space Administration ;, 1974), by William Roger Russin and Langley Research Center (page images at HathiTrust)
• Comparison of combustion characteristics of ASTM A-1, propane, and natural-gas fuels in an annular turbojet combustor (National Aeronautics and Space Administration ;, 1973), by Jerrold D. Wear, Robert E. Jones, and Lewis Research Center (page images at HathiTrust)
• Performance of a modular combustor designed for a VTOL tip-turbine lift fan (National Aeronautics and Space Administration :, 1971), by Nicholas R. Marchionna, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6352 (National Aeronautics and Space Administration:, 1971), by Robert E. Jones (page images at HathiTrust; US access only)
• Correlation of secondary sonic and supersonic gaseous jet penetration into supersonic crossflows (National Aeronautics and Space Administration ;, 1971), by Frederick P. Povinelli, Louis A. Povinelli, and Lewis Research Center (page images at HathiTrust)
• Seven commercial organo-metallic additives (National Advisory Committee for Aeronautics, 1954), by Vincent F. Hlavin, William P. Cook, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Examination of smoke and carbon from turbojet-engine combustors (National Advisory Committee for Aeronautics, 1952), by Thomas P. Clark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Experimental investigation of a lightweight rocket chamber (National Advisory Committee for Aeronautics, 1953), by John E. Dalgleish, Adelbert O. Tischler, United States National Advisory Committee for Aeronautics, and Lewis Flilght Propulsion Laboratory (page images at HathiTrust)
• Effect of fuel additives on carbon deposition in a J33 single combustor [Part] 1, Three metallic-organic additives (National Advisory Committee for Aeronautics, 1952), by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Performance investigation of can-type combustor from British turbojet engine and comparison of this combustor with can-type combustor from U.S. turbojet engine (National Advisory Committee for Aeronautics, 1950), by William P. Cook, Richard G. Koch, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Vapor-fuel-distribution effects on combustion performance of a single tubular combustor (National Advisory Committee for Aeronautics, 1950), by Richard J. McCafferty, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Calculations of the performance of a compression-ignition engine-compressor turbine combination. [Part] 2, Performance of complete combination (National Advisory Committee for Aeronautics, 1947), by Alexander Mendelson, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• Combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), by Bemrose Boyd, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• A study of liquid boric oxide particle growth rates in a gas stream from a simulated jet engine combustor (National Advisory Committee for Aeronautics, 1957), by Paul C. Setze, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas (National Advisory Committee for Aeronautics, 1957), by Charles C. Graves, Jack S. Grobman, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine (National Advisory Committee for Aeronautics, 1952), by Joseph H. Judd, Otto F. Trout, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Low-pressure performance of different diameter experimental combustor liners (National Advisory Committee for Aeronautics, 1954), by Ralph T. Dittrich, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Effect of combustor-inlet conditions on performance of an annular turbojet combustor (National Advisory Committee for Aeronautics, 1947), by J. Howard Childs, Oakley W. Surine, RIchard J. McCafferty, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Knocking combustion observed in a spark-ignition engine with simultaneous direct and schlieren high-speed motion pictures and pressure records (National Advisory Committee for Aeronautics, 1948), by Gordon E. Osterstrom and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effects of fuel-nozzle carbon deposition on combustion efficiency of single tubular-type, reverse-flow turbojet combustor at simulated altitude conditions (National Advisory Committee for Aeronautics, 1948), by Ralph T. Dittrich and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by J. C. Sanders, Alexander Mendelson, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Experimental study of the effects of elevated pressure and temperature on jet mixing and emissions in an RQL combustor for stable, efficient and low emissions gas turbine applications : final project report (California Energy Commission, 2012), by G. S Samuelsen, V. G McDonell, V Jermakian, Irvine. Advanced Power and Energy Program University of California, and California Energy Commission. Public Interest Energy Research (page images at HathiTrust)

More items available under broader and related terms at left.