The Online Books Page

Airplanes -- Turbojet engines -- Combustion -- Equipment and supplies -- Testing

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

• Airplanes -- Turbojet engines -- Combustion -- Equipment and supplies
• Airplanes -- Turbojet engines -- Testing
• Combustion -- Testing

• 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)

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

• Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), by Verlon L. Head, William H. Gerstenmaier, Louis A. Povinelli, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Design and cold-air test of single-stage uncooled core turbine with high work output (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Thomas P. Moffitt, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Noise generated by quiet engine fans : III - fan C (U.S. National Aeronautics and Space Administration ;, 1976), by Francis J. Montegani, Ralph F. Schmiedlin, John W. Schaefer, and Lewis Research Center (page images at HathiTrust)
• Mach 4 free-jet tunnel-starting experiments for a hypersonic research engine model causing high blockage (National Aeronautics and Space Administration ;, 1976), by George T. Carson, Raymond E. Midden, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A method for obtaining practical flutter-suppression control laws using results of optimal control theory (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Jerry R. Newsom, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Altitude calibration of an F100, S/N P680063, turbofan engine (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Thomas J. Biesiadny, Jose R. Rodriguez, Douglas Lee, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Performance of a J85-13 compressor with clean and distorted inlet flow (National Aeronautics and Space Administration ;, 1975), by Edward J. Milner, Leon M. Wenzel, and Lewis Research Center (page images at HathiTrust)
• Performance of two tangential jet blades (National Aeronautics and Space Administration ;, 1970), by James L. Bettner, Lewis Research Center, and General Motors Company (page images at HathiTrust)
• Exhaust emission calibration of two J-58 afterburning turbojet engines at simulated high-altitude, supersonic flight conditions (U.S. National Aeronautics and Space Administration ;, 1976), by J. D. Holdeman and Lewis Research Center (page images at HathiTrust)
• Turbine for a low-cost turbojet engine (National Aeronautics and Space Administration ;, 1974), by Milton G. Kofskey, U.S. Army Air Mobility Research and Development Laboratory, and Lewis Research Center (page images at HathiTrust)
• Investigation of acceleration characteristics of a single-spool turbojet engine (National Advisory Committee for Aeronautics, 1953), by Frank L. Oppenheimer, George J. Pack, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Experimental cooling-air impeller performance and turbine rotor temperatures in modified J33 split-disk rotor up to speeds of 10,000 RPM (National Advisory Committee for Aeronautics, 1952), by Alfred J. Nachtigall, Robert R. Ziemer, Charles F. Zalabak, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air (National Advisory Committee for Aeronautics, 1950), by Eugene V. Zettle, Herman Mark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Transient operating characteristics of a turbojet engine when subjected to step changes in fuel flow (National Advisory Committee for Aeronautics, 1950), by Arthur H. Bell, J. Elmo Farmer, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Over-all engine performance (National Advisory Committee for Aeronautics, 1948), by J. C. Nettles, J. R. Easterly, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust; US access only)
• Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Natural icing of an axial-flow turboject engine in flight for a single icing condition (National Advisory Committee for Aeronautics, 1948), by Loren W. Acker, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Performance of J33 turbojet engine with shaft-power extraction [Part] 2, Compressor (National Advisory Committee for Aeronautics, 1948), by Albert O. Ross, J. Cary Nettles, J. R. Easterly, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust; US access only)

• Experimental evaluation of a Mach 3.5 axisymmetric inlet (National Aeronautics and Space Administration ;, 1975), by J. Syberg, J. L. Koncsek, Ames Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• NASA TN D-3929 (National Aeronautics and Space Administration ;, 1967), by Jimmy M. Cawthorn, Clyde Hayes, Garland J. Morris, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)

• Fluctuating pressures on fan blades of a turbofan engine : flight test investigation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by James A. Schoenster and Langley Research Center (page images at HathiTrust)

• Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine (National Advisory Committee for Aeronautics, 1955), by Reeves P. Cochran, Robert P. Dengler, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• Bonding and compatibility of aluminum oxide fibers in nickel alloy composites (National Aeronautics and Space Administration ;, 1976), by Leonard J. Westfall and Lewis Research Center (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)

• Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine (National Advisory Committee for Aeronautics, 1955), by Reeves P. Cochran, Robert P. Dengler, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Evaluation of a compressor bleed system for rim cooling the turbine wheel of a turbojet engine (National Advisory Committee for Aeronautics, 1954), by C. R. Morse, R. H. Kemp, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• Experimental investigation of external water-spray cooling in a turbojet engine utilizing several injection configurations including orifices in the rotor-blade bases (National Advisory Committee for Aeronautics, 1955), by Roy A. McKinnon, John C. Freche, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Fabrication and endurance of air-cooled strut-supported turbine blades with struts cast of X-40 alloy (National Advisory Committee for Aeronautics, 1956), by Eugene F. Schum, Robert E. Oldrieve, Francis S. Stepka, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Analytical and experimental investigation of a forced-convection air-cooled internal strut-supported turbine blade (National Advisory Committee for Aeronautics, 1954), by Eugene F. Schum, Francis S. Stepka, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• Development of acoustically lined ejector technology for multitube jet noise suppressor nozzles by model and engine tests over a wide range of jet pressure ratios and temperatures (National Aeronautics and Space Administration ;, 1974), by J. Atvars, Lewis Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)

• NASA TN D-3929 (National Aeronautics and Space Administration ;, 1967), by Jimmy M. Cawthorn, Clyde Hayes, Garland J. Morris, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)

• NASA TN D-4141 (National Aeronautics and Space Administration ;, 1967), by Terrell W. Feistel, Robert C. Innis, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)

• Determination of microgram quantities of carbon by low-pressure combustion (Oak Ridge National Laboratory, 1957), by J. H. Edgerton, H. G. Davis, U.S. Atomic Energy Commission, and Oak Ridge National Laboratory. Analytical Chemistry Division (page images at HathiTrust)
• NASA TN D-6523 (National Aeronautics and Space Administration :, 1971), by Thomas H. Cochran, Lewis Research Center, and United States National Aeronautics and Space Administration (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)

• NASA TN D-6523 (National Aeronautics and Space Administration :, 1971), by Thomas H. Cochran, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of diffusion flame tests (Sandia National Laboratories, 1987), by J. E. Shepherd, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Reactor Accident Analysis, Sandia National Laboratories, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering (page images at HathiTrust)

• NASA TN D-6287 (National Aeronautics and Space Administration ;, 1971), by Marcus F. Heidmann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

• Auto-ignition and combustion of diesel fuel in a constant-volume bomb (National Advisory Committee for Aeronautics, 1938), by Robert F. Selden and Langley Aeronautical Laboratory (page images at HathiTrust)
• Electrical characteristics of spark generators for automotive ignition (National Advisory Committee for Aeronautics, 1926), by R. B. Brode, F. B. Silsbee, D. W. Randolph, and Langley Aeronautical Laboratory (page images at HathiTrust)

• Chemical-kinetic basis for differentiation of secondary and priming explosives (National Aeronautics and Space Administration, 1966), by K. K. Andreev, M. S. Pli︠a︡sunov, and Vsesoi︠u︡znoe khimicheskoe obshchestvo im. D.I. Mendeleeva (page images at HathiTrust)

• Methods of evaluating explosive reactivity of explosive-contaminated solid waste substances (U.S. Dept. of the Interior, Bureau of Mines, 1988), by T. S. Bajpayee and Richard J. Mainiero (page images at HathiTrust)

• Detonability of H2-air diluent mixtures (Division of Reactor System Safety, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission., 1987), by Sheldon R. Tieszen and U.S. Nuclear Regulatory Commission. Division of Reactor System Safety (page images at HathiTrust; US access only)
• Analysis of diffusion flame tests (Sandia National Laboratories, 1987), by J. E. Shepherd, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Reactor Accident Analysis, Sandia National Laboratories, and U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering (page images at HathiTrust)

• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), by Harvey A. Cook, W. T. Olson, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Interrelation of exhaust-gas constituents (National Advisory Committee for Aeronautics, 1938), by Harold C. Gerrish, Fred Voss, and Langley Aeronautical Laboratory (page images at HathiTrust)

• Preliminary evaluation of bit impact ignitions of methane using a drum-type cutting head (U.S. Dept. of the Interior, Bureau of Mines, 1982), by Wallance W. Roepke, Carl F. Wingquist, V. William Dellorfano, and David A. Larson (page images at HathiTrust)

• NASA TN D-5214 (National Aeronautics and Space Administration ;, 1969), by D. E. Sokolowski, E. William Conrad, David W. Vincent, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

More items available under broader and related terms at left.