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Combustion chambers

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• Internal combustion engines

• Aircraft gas-turbines -- Combustion chambers
• Gas-turbines -- Combustion chambers
• Jet engines -- Combustion chambers

• Chambers, Combustion
• Combustors

• Conventionally cast and forged copper alloy for high-heat-flux thrust chambers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by John M. Kazaroff, George A. Repas, and Lewis Research Center (page images at HathiTrust)
• Effect of propellant-feed-system coupling and hydraulic parameters on analysis of chugging / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Don J. Wood, Robert G. Dorsch, and Lewis Research Center (page images at HathiTrust)
• Program user's manual for optimizing the design of a liquid or gaseous propellant rocket engine with the automated combustor design code AUTOCOM / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by R. H. Reichel, Lewis Research Center, and Aerophysics Research Corporation (page images at HathiTrust)
• Effect of primary-zone water injection on pollutants from a combustor burning liquid ASTM A-1 and vaporized propane fuels / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Robert D. Ingebo, Carl T. Norgren, and Lewis Research Center (page images at HathiTrust)
• Propellant vaporization as a design criterion for rocket-engine combustion chambers / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1960), by Richard J. Priem, Marcus F. Heidmann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Reliability and effective thermal conductivity of three metallic-ceramic composite insulating coatings on cooled hydrogen-oxygen rockets / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Harold G. Price, Richard J. Quentmeyer, Ralph L. Schacht, and Lewis Research Center (page images at HathiTrust)
• Performance of a hydrogen burner to simulate air entering scramjet combustors / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by William Roger Russin and Langley Research Center (page images at HathiTrust)
• Evaluation of a thin-film, heat-flux probe for measuring gas velocities in an unstable rocket combustor / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Frederick P. Povinelli, Robert D. Ingebo, and Lewis Research Center (page images at HathiTrust)
• Technique for predicting high-frequency stability characteristics of gaseous-propellant combustors / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Richard J. Priem, Jefferson Y. S. Yang, and Lewis Research Center (page images at HathiTrust)
• Afterburner performance of circular v-gutters and a sector of parallel v-gutters for a range of inlet temperatures to 1255 K (1800 ̊F) / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by J. Robert Branstetter, Gregory M. Reck, and Lewis Research Center (page images at HathiTrust)
• A preliminary investigation of oxidizer-rich oxygen-hydrogen combustion characteristics / (Washington, D.C. : 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)
• High-pressure combustor exhaust emissions with improved air-atomizing and conventional pressure-atomizing fuel nozzles (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Robert D. Ingebo, Carl T. Norgren, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Simultaneous film and convection cooling of a plate inserted in the exhaust stream of a gas turbine combustor (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Cecil J. Marek, Albert J. Juhasz, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Comparison of combustion characteristics of ASTM A-1, propane, and natural-gas fuels in an annular turbojet combustor / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Jerrold D. Wear, Robert E. Jones, and Lewis Research Center (page images at HathiTrust)
• Turbulent heat-transfer prediction method for application to scramjet engines / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by S. Z. Pinckney and Langley Research Center (page images at HathiTrust)
• Nonreactive mixing study of a scramjet swept-strut fuel injector / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Charles R. McClinton and Langley Research Center (page images at HathiTrust)
• Sonotech, Inc. frequency-tunable pulse combustion system (Cello Pulse Burner) : innovative technology evaluation report. (Cincinnati, Ohio : 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)
• H. Walter Kommanditgesellschaft - catapult experiments - mine detonations / (Washington, D.C. : Office of the Publication Board, Dept. of Commerce, [1945]), by W. J. Woodward, E. V. Dahl, R. R. Witter, and United States. Publication Board (page images at HathiTrust)
• Effect of exit temperature sampling density on measured combustor performance / (Washington, D.C.: National Aeronautics and Space Administration:, 1971), by Robert E. Jones (page images at HathiTrust; US access only)
• Stability limits and efficiency of swirl-can combustor modules burning natural gas fuel / (Washington, D.C. : 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)
• Effect of hydrogen injection stability and emissions of an experimental premixed prevaporized propane burner / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 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 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• Jet model for slot film cooling with effect of free-stream and coolant turbulence / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Frederick F. Simon and Lewis Research Center (page images at HathiTrust)
• Development of a barium chemical release system / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by C. S. Stokes, W. J. Murphy, E. W. Smith, Temple University, and Langley Research Center (page images at HathiTrust)
• Experimental determination of the temperature and dynamic-strain environment of a tubular combustor liner in a turbojet engine / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Patrick T. Chiarito, C. Robert Morse, William C. Morgan, and Lewis Research Center (page images at HathiTrust)
• Magnetic control of the flow of hot combustion gases in hydrogen-oxygen combustion at 14 atmospheres / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Ronald Razner and Lewis Research Center (page images at HathiTrust)
• Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Arthur N. Curren and Lewis Research Center (page images at HathiTrust)
• Determination of primary-zone smoke concentrations from spectral radiance measurements in gas turbine combustors / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Carl T. Norgren, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preliminary investigation of diffuser wall bleed to control combustor inlet airflow distribution / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Albert J. Juhasz, J. D. Holdeman, 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 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Martin Hersch, Edward J. Rice, 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 / (Washington, [D.C.] : 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)
• Drag and distribution measurements of single-element fuel injectors for supersonic combustors / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Louis A. Povinelli and Lewis Research Center (page images at HathiTrust)
• Preliminary tests of a simplified modular turbojet combustor / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Richard W. Niedzwiecki, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Relation of emitted ultraviolet radiation to combustion of hydrogen and oxygen at 20 atmospheres / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Marshall C. Burrows, Ronald Razner, and Lewis Research Center (page images at HathiTrust)
• Radiation processes related to oxygen-hydrogen combustion at high pressures / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Marshall C. Burrows and Lewis Research Center (page images at HathiTrust)
• Performance of swirl-can turbojet combustors at simulated supersonic combustor-inlet conditions / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 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. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert D. Ingebo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of a modular combustor designed for a VTOL tip-turbine lift fan / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1971]), by Nicholas R. Marchionna, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Correlation of secondary sonic and supersonic gaseous jet penetration into supersonic crossflows / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1971]), by Frederick P. Povinelli, Louis A. Povinelli, and Lewis Research Center (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 / ([Sacramento, Calif.] : 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)
• Examination of smoke and carbon from turbojet-engine combustors / (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by Thomas P. Clark, United States. National Advisory Committee for Aeronautics. NACA research memorandum, 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1950]), by Richard J. McCafferty, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Calculations of the performance of a compression-ignition engine-compressor turbine combination. (Washington, D.C. : National Advisory Committee for Aeronautics, [1947]), by Alexander Mendelson, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Joseph H. Judd, Otto F. Trout, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Performance comparisons of JFC-2 and MIL-F-5624A (JP-3) fuels in tubular and annular combustors / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Richard J. McCafferty, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Effect of fuel additives on carbon deposition in a J33 single combustor (Washington, D.C. : National Advisory Committee for Aeronautics, [1954]), by Vincent F. Hlavin, William P. Cook, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Experimental investigation of a lightweight rocket chamber / (Washington, D.C. : National Advisory Committee for Aeronautics, [1953]), by John E. Dalgleish, Adelbert O. Tischler, United States. National Advisory Committee for Aeronautics. NACA research memorandum, 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 (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, United States. National Advisory Committee for Aeronautics. NACA research memorandum, 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 / (Washington : National Advisory Committee for Aeronautics, [1950]), by William P. Cook, Richard G. Koch, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Altitude-wind-tunnel investigation of Westinghouse 19B-2 19B-8, and 19XB-1 jet-propulsion engines (Washington, D.C. : National Advisory Committee for Aeronautics, [1948]), by Bemrose Boyd, United States. National Advisory Committee for Aeronautics. NACA research memorandum, 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1957]), by Paul C. Setze, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, 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/ (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Charles C. Graves, Jack S. Grobman, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Low-pressure performance of different diameter experimental combustor liners / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Ralph T. Dittrich, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Effect of combustor-inlet conditions on performance of an annular turbojet combustor / (Washington, D.C. : 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 / (Washington, D.C. : 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 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by Ralph T. Dittrich and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Calculations of the performance of a compression-ignition engine-compressor turbine combination. 1 - Performance of a highly supercharged compression-ignition engine / (Washington, D.C. : 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)

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