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Airplanes -- Turbojet engines -- Mathematical models

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• Airplanes -- Turbojet engines
• Airplanes -- Mathematical models

• Airplanes -- Turbojet engines -- Computer simulation
• Airplanes -- Turbojet engines -- Air intakes -- Mathematical models

• Performance potential of an advanced technology Mach 3 turbojet engine installed on a conceptual high-speed civil transport (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by Shelby J. Morris, Peter G. Coen, Karl A. Geiselhart, and Langley Research Center (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)

• Program for calculating linear A, B, C, and D matrices from a nonlinear dynamic engine simulation (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978), by Lucille C. Geyser (page images at HathiTrust)
• HYDES : a generalized hybrid computer program for studying turbojet or turbofan engine dynamics (National Aeronautics and Space Administration ;, 1974), by John R. Szuch and Lewis Research Center (page images at HathiTrust)

• Analysis of a stability valve system for extending the dynamic range of a supersonic inlet (National Aeronautics and Space Administration ;, 1975), by John A. Webb, Miles O. Dustin, and Lewis Research Center (page images at HathiTrust)
• Analysis of pressure distortion testing (National Aeronautics and Space Administration ;, 1976), by K. E. Koch, R. L. Rees, General Electric Company, and Lewis Research Center (page images at HathiTrust)

• Analytical investigation of fan tone noise due to ingested atmospheric turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Ulrich W. Ganz, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust)
• Use of potential flow theory to evaluate subsonic inlet data from a simulator-powered nacelle at cruise conditions (National Aeronautics and Space Administration ;, 1974), by Lawrence J. Bober and Lewis Research Center (page images at HathiTrust)

• Combined quadrupole-dipole model for inlet flow distortion noise from a subsonic fan (National Aeronautics and Space Administration ;, 1974), by Marvin E. Goldstein, Thomas F. Gelder, James H. Dittmar, and Lewis Research Center (page images at HathiTrust)
• Optimal one-section and two-section circular sound-absorbing duct liners for plane-wave and monopole sources without flow (National Aeronautics and Space Administration ;, 1976), by Harold C. Lester, Joe W. Posey, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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

• Turbine engine particulate emission characterization (Dept. of Transportation, Federal Aviation Administration, Systems Research and Development Service ;, 1977), by Donald L. Fenton, Erdmann H Luebcke, Eric W Nordstrom, and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
• Gas turbines for aircraft (McGraw-Hill Book Co., 1949), by F. W. Godsey and Lloyd Arthur Young (page images at HathiTrust)
• Aircraft gas turbines. (Wiley, 1956), by Chester Warren Smith (page images at HathiTrust)
• Gas turbines for aircraft (Ronald Press Co., 1955), by Ivan Howard Driggs and Otis E. Lancaster (page images at HathiTrust)
• FT4 gas turbine engine installation handbook. ([East Hartford, Conn.], 1963), by United Aircraft Corporation. Pratt & Whitney Aircraft Division (page images at HathiTrust)
• FT3C gas turbine engine installation handbook. ([East Hartford, Conn.], 1963), by United Aircraft Corporation. Pratt & Whitney Aircraft Division (page images at HathiTrust)
• NACA Conference on Turbojet-Engine Thrust-Augmentation Research; a compilation of the papers presented by NACA staff members, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, October 28, 1948. ([Washington?, 1948), by United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Oversight of FAA--reliability of "drilled" turbine fan blades on CF-6 engine used to power DC-10 and A-300B aircraft hearings before the Special Subcommittee on Investigations of the Committee on Interstate and Foreign Commerce, House of Representatives, Ninety-third Congress, second session ... July 2 and 10, 1974. (U.S. Govt. Print. Off., 1975), by United States. Congress. House. Committee on Interstate and Foreign Commerce. Special Subcommittee on Investigations (page images at HathiTrust)
• Simulator for use in development of jet engine controls. (U.S. Dept. of Commerce, National Bureau of Standards, 1957), by Emile S. Sherrard (page images at HathiTrust)
• Technical papers. (Federal Aviation Agency, Systems Research & Development Service, Office of International Aviation, 1964), by Atlantic City International Aviation R & D Symposium: All-Weather Landing Systems. 2d (page images at HathiTrust)
• Proceedings [held] April 16-19, 1963. (Aeronautical Systems Division, Air Force Systems Command;, 1963), by USAF Aerospace Fluids and Lubricants Conference (1963 : San Antonio), Pei Moo Ku, and San Antonio Southwest Research Institute (page images at HathiTrust)
• Safety and acoustic factors in the operation of turbojet and turbofan aircraft at Newark Airport (Cornell Aeronautical Laboratory, 1961), by Murray Kamrass (page images at HathiTrust)
• Proceedings [held] April 16-19, 1963. (AF Materials Laboratory, Research and Technology Division, Air Force Systems Command; [obtainable from the Defense Documentation Center, Alexandria, Va.], 1964), by USAF Aerospace Fluids and Lubricants Conference (1963 : San Antonio), R. L. Adamczak, and San Antonio Southwest Research Institute (page images at HathiTrust)
• Minimal manoeuvres of high performance aircraft in a vertical plane. (Purdue University, School of Aeronautical Engineering, 1958), by Angelo Miele (page images at HathiTrust)
• Approximate solutions to optimum flight trajectories for a turbo-jet powered aircraft (Purdue University, School of Aeronautical Engineering, 1957), by Angelo Miele and James O. Cappellari (page images at HathiTrust)
• Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds (National Aeronautics and Space Administration ;, 1974), by Roger Chamberlin and Lewis Research Center (page images at HathiTrust)
• Conceptual study of a turbojet/ramjet inlet (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by John P. Weidner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Prediction of axial-flow instabilities in a turbojet engine by use of a multistage compressor simulation on the digital computer (National Aeronautics and Space Administration ;, 1975), by Carl J. Daniele, Kurt Seldner, Ronald J. Blaha, and Lewis Research Center (page images at HathiTrust)
• Analysis of a topping-cycle, aircraft, gas-turbine-engine system which uses cryogenic fuel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by George E. Turney, Laurence H. Fishbach, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight investigation of installation effects on a plug nozzle with a series of boattailed primary shrouds installed on an underwing nacelle (National Aeronautics and Space Administration ;, 1974), by Verlon L. Head and Lewis Research Center (page images at HathiTrust)
• Overall and blade-element performance of a 1.20-pressure-ratio fan stage at design blade setting angle (National Aeronautics and Space Administration ;, 1974), by George W. Lewis, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
• Effect of slotted casing treatment on performance of a multistage compressor (National Aeronautics and Space Administration ;, 1976), by John E. Moss and Lewis Research Center (page images at HathiTrust)
• Altitude performance of a low-noise-technology fan in a turbofan engine with and without a sound suppressing nacelle (U.S. National Aeronautics and Space Administration ;, 1976), by Thomas J. Biesiadny, Mahmood Abdelwahab, Rudolph E. Grey, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Small, low-cost, expendable turbojet engine : II - performance characteristics (National Aeronautics and Space Administration ;, 1976), by Robert P. Dengler, Lawrence E. Macioce, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of calculated and altitude-facility-measured thrust and airflow of two prototype F100 turbofan engines (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Frank J. Kurtenbach, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effect of slotted casing treatment with change in Reynolds number index on performance of a jet engine (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by John E. Moss, Willis M. Braithwaite, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Flight investigation of installation effects on a wedge nozzle installed on an underwing nacelle (National Aeronautics and Space Administration ;, 1975), by Albert L. Johns and Lewis Research Center (page images at HathiTrust)
• Effect of a simulated engine jet blowing above an arrow wing at mach 2.0 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Barrett L. Shrout, Clyde Hayes, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effect of screen-induced total-pressure distortion on axial-flow compressor stability (National Aeronautics and Space Administration ;, 1974), by James E. Calogeras, Paul L. Burstadt, Roy L. Johnsen, and Lewis Research Center (page images at HathiTrust)
• Comparison of cooling effectiveness of turbine vanes with and without film cooling (National Aeronautics and Space Administration ;, 1974), by Frederick C. Yeh and Lewis Research Center (page images at HathiTrust)
• Small, Low-cost, expendable turbojet engine : I - design, fabrication, and preliminary testing (U.S. National Aeronautics and Space Administration ;, 1976), by Robert P. Dengler, Lawrence E. Macioce, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Spectral radiance measurements and calculated soot concentrations along the length of an experimental combustor (U.S. National Aeronautics and Space Administration ;, 1976), by Carl T. Norgren, Robert D. Ingebo, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effect of casing treatment on performance of a multistage compressor (National Aeronautics and Space Administration ;, 1975), by Leon M. Wenzel, Charles M. Mehalic, John E. Moss, and Lewis Research Center (page images at HathiTrust)
• Evaluation of a simplified gross thrust calculation technique using two prototype F100 turbofan engines in an altitude facility (National Aeronautics and Space Administration, Scientific and Technical Information Branch :, 1979), by Frank J. Kurtenbach, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerodynamic performance of 0.4066-scale model of JT8D refan stage (U.S. National Aeronautics and Space Administration ;, 1976), by Royce D. Moore, Edward R. Tysl, George Kovich, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude (National Aeronautics and Space Administration Scieentific and Technical Information Branch ;, 1983), by David M. Straight, Richard R. Cullom, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• An application of theory to axial compressor noise (National Aeronautics and Space Administration, 1970), by J. B. Ollerhead, C. L. Munch, United States National Aeronautics and Space Administration, Langley Research Center, and Wyle Laboratories (page images at HathiTrust)
• Literature search of publications concerning the prediction of dynamic inlet flow distortion and related topics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by William G. Schweikhard, Yen-Sen Chen, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Factors that affect operational reliability of turbojet engines (U.S. G.P.O.], 1960), by Lewis Center Staff (page images at HathiTrust)
• NASA TN D-6021 (National Aeronautics and Space Administration :, 1971), by Francis J. Paulovich, Ralph E. Hagedorn, George H. Neiner, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5928 (National Aeronautics and Space Administration :, 1970), by David G. Evans, Francis S. Stepka, Keith A. Furgalus, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of effect of propulsion system installation and operation on aerodynamics of an airbreathing hypersonic airplane at Mach O.3 to 1.2 (National Aeronautics and Space Administration ;, 1977), by James M. Cubbage, Charles E. Mercer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5993 (National Aeronautics and Space Administration :, 1971), by Mark H. Waters and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Turbojet-engine noise studies to evaluate effects of inlet-guide-vane--rotor spacing (National Aeronautics and Space Administration, 1968), by John L. Crigler, Garland J. Morris, W. Latham Copeland, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of several methane-fueled engine cycles for Mach 3.0 flight (National Aeronautics and Space Administration ;, 1968), by Brent A. Miller, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamic performance of 0.4066-scale model of JT8D refan stage with S-duct inlet (National Aeronautics and Space Administration ;, 1977), by Royce D. Moore, George W. Lewis, George Kovich, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5672 (National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by James S. Fear, Robert R. Tacina, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6404 (National Aeronautics and Space Administration ;, 1971), by Daniel Briehl, Leonidas Papathakos, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Sound radiation from a high-speed axial-flow fan due to the inlet turbulence quadrupole interaction (National Aeronautics and Space Administration ;, 1974), by Marvin E. Goldstein, Lynn U. Albers, Burt M. Rosenbaum, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-1801 (National Aeronautics and Space Administration, 1963), by Paul A. Hunter, Mary W. Fetner, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• 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)
• Dispersion of turbojet engine exhaust in flight (National Aeronautics and Space Administration ;, 1973), by James D. Holdeman and Lewis Research Center (page images at HathiTrust)
• Flight monitor for jet engine disk cracks and the use of critical length criterion of fracture mechanics (National Aeronautics and Space Administration ;, 1973), by John P. Barranger and Lewis Research Center (page images at HathiTrust)
• Inlet noise suppressor performance with a turbojet engine as the noise source (National Aeronautics and Space Administration, 1971), by John F. Groeneweg, Charles E. Feiler, Loren W. Acker, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of basic XJ79-GE-1 turbojet engine and its components. (National Advisory Committee for Aeronautics, 1961), by Carl E. Campbell and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Performance of basic XJ79-GE-1 turbojet engine and its components (National Advisory Committee for Aeronautics, 1958), by Carl E. Campbell and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Preliminary investigation of the strength and endurance of plastic-impregnated fiberglass compressor blades (National Advisory Committee for Aeronautics, 1955), by Donald F. Johnson, Andre J. Meyer, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Endurance evaluation of shell-supported turbine rotor blades made of timken 17-22A (S) steel (National Advisory Committee for Aeronautics, 1951), by Francis S. Stepka, John L. Clure, H. Robert Bear, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Photographic studies of preignition environment and flame initiation in turbojet-engine combustors (National Advisory Committee for Aeronautics, 1953), by David M. Straight, J. Dean Gernon, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Investigation of combustion screech and a method of its control (National Advisory Committee for Aeronautics, 1954), by James L. Jr Harp, Lively Bryant, Wallace W. Velie, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (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)
• Carbon deposition obtained with MIL-F-5624A fuels in a single combustor and in three full-scale engines (National Advisory Committee for Aeronautics, 1954), by Jerrold D. Wear, 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)
• Photographic investigation of air-flow patterns in transparent one-sixth sector of annular turbojet-engine combustor with axial-slot-type air admission (National Advisory Committee for Aeronautics, 1954), by Charles C. Graves, J. Dean Gernon, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Relation of turbine-engine combustion efficiency to second-order reaction kinetics and fundamental flame speed (National Advisory Committee for Aeronautics, 1954), by J. Howard Childs, Charles C. Graves, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Low-pressure performance of experimental prevaporizing tubular combustor using approximately stoichiometric admission of fuel-air mixture into the primary zone (National Advisory Committee for Aeronautics, 1954), by Robert R. Hibbard, Wilfred E. Scull, Allen J. Metzler, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Engine design-point performance (National Advisory Committee for Aeronautics, 1954), by James E. Hubbartt, Wilson B. Schramm, R. J. Rossbach, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Determination of surge and stall limits of an axial-flow turbojet engine for control applications (National Advisory Committee for Aeronautics, 1953), by Ross D. Schmidt, Edward W. McGraw, George Vasu, 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)
• Carbon deposition of several special turbojet-engine fuels (National Advisory Committee for Aeronautics, 1951), by Jerrold D. Wear, James W. Useller, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Effects of special leading- and trailing-edge modifications on blade temperature (National Advisory Committee for Aeronautics, 1951), by Herman H. Ellerbrock, Gordon T. Smith, Charles F. Zalabak, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Rotor blades with 34 steel tubes in cooling-air passages (National Advisory Committee for Aeronautics, 1950), by Robert O. Hickel, Gordon T. Smith, 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)
• 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)
• Endurance evaluation of several tube-filled rotor blades (National Advisory Committee for Aeronautics, 1952), by Jack B. Esgar, John L. Clure, 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)
• Conduction and film cooling of leading and trailing edges of rotor blades (National Advisory Committee for Aeronautics, 1951), by Vernon L. Arne, Jack B. Esgar, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Rotor blades with split trailing edges (National Advisory Committee for Aeronautics, 1951), by Gordon T. Smith, Robert O. Hickel, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Combustion efficiency and altitude operational limits of three liquid hydrocarbon fuels having high volumetric energy content in a J33 single combustion (National Advisory Committee for Aeronautics, 1950), by Edward G. Stricker and United States National Advisory Committee for Aeronautics (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)
• Effect of fuels and fuel-nozzle characteristics on performance of an annular combustor at simulated altitude conditions (National Advisory Committee for Aeronautics, 1948), by RIchard J. McCafferty, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• An analysis of control requirements and control parameters for direct-coupled turbojet engines (National Advisory Committee for Aeronautics, 1948), by David Novik, Edward W. Otto, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Jet diffuser for simulating ram conditions on a turbojet-engine static test stand (National Advisory Committee for Aeronautics, 1947), by Robert H. Essig, David S. Gabriel, H. R. Bohanon, United States National Advisory Committee for Aeronautics, and Aircraft Engine 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)
• An analog study of a shock-position diffuser control on a supersonic turbojet engine (National Advisory Committee for Aeronautics, 1956), by David Novik, 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)
• Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination (National Advisory Committee for Aeronautics, 1958), by J. Cary Nettles, Robert C. Campbell, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Design and evaluation of a turbojet-exhaust simulator with a solid-propellant rocket motor for free-flight research (National Advisory Committee for Aeronautics, 1957), by Abraham Leiss, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Fuel characteristics pertinent to the design of aircraft fuel systems. Supplement 1 - Additional information on MIL-F-7914(AER) Grade JP-5 fuel and several fuel oils (National Advisory Committee for Aeronautics, 1953), by Henry C. Barnett, Robert R. Hibbard, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Component performance investigation of J71 experimental turbine. [Part] V, Effect of third stage shrouding on internal-flow conditions of J71-97 turbine (National Advisory Committee for Aeronautics, 1956), by Donald A. Petrash, Elmer H. Davison, Harold J. Schum, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Generalization of turbojet-engine performance in terms of pumping characteristics (National Advisory Committee for Aeronautics, 1949), by Newell D. Sanders, Michael Behun, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of heat and power extraction on turbojet-engine performance. 4 - Analytical determination of effects of hot-gas bleed (National Advisory Committee for Aeronautics, 1951), by Stanley L. Koutz and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The near noise field of static jets and some model studies of devices for noise reduction (National Advisory Committee for Aeronautics, 1954), by Leslie W. Lassiter, Harvey H. Hubbard, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 (National Aeronautics and Space Administration, 1960), by David N. Bowditch, William K. Tabata, Bernhard H. Anderson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of afterbody terminal fairings on the performance of a pylon-mounted turbojet-nacelle model (National Aeronautics and Space Administration, 1960), by Conrad M. Willis, Charles E. Mercer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preliminary evaluation of turbine performance with variable-area turbine nozzles in a turbojet engine (National Advisory Committee for Aeronautics, 1960), by Carl E. Campbell, Henry J. Welna, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Model specification: engine, aircraft, turbojet, J69-T-25 (Continential Model 352-5A) Specification No. 2149. (Detroit, 1958), by Detroit Continental Aviation and Engineering Corporation (page images at HathiTrust; US access only)
• Preliminary model specification, turbojet aircraft engine, continental model CJ69-1400. (Detroit, 1960), by Detroit Continental Aviation and Engineering Corporation (page images at HathiTrust; US access only)
• The US Army Transportation School Apprenticeship Program for the trade of aircraft engine mechanic (turbine). (Dept. of Defense, Dept. of the Army, Headquarters, 1978), by United States. Department of the Army and US Army Transportation School (page images at HathiTrust)
• Proceedings (AF Materials Laboratory, Research and Technology Division, Air Force Systems Command, Wright-Patterson Air Force Base, 1964), by USAF Aerospace Fluids and Lubricants Conference (1963 : San Antonio) and R. L. Adamczak (page images at HathiTrust; US access only)
• A balanced-pressure sliding seal for transfer of pressurized air between stationary and rotating parts (National Advisory Committee for Aeronautics, 1957), by Arthur N. Curren, Reeves P. Cochran, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Meteorological problems associated with commercial turbo-jet aircraft operation (National Advisory Committee for Aeronautics, 1955), by United States. National Advisory Committee for Aeronautics. Subcommittee on Meteorological Problems (page images at HathiTrust; US access only)
• Performance of turbojet inlets (United Aircraft Corp., Research Dept., 1955), by George McLafferty and United Aircraft Corporation. Research Dept (page images at HathiTrust; US access only)
• Jet engine accident investigation (Flight Propulsion Division, General Electric, 1959), by General Electric Company. Flight Propulsion Division. Service Training School (page images at HathiTrust; US access only)
• Jet power : a history of jet engine progress at General Electric. (The Company, 1958), by General Electric Company. Aircraft Gas Turbine Development Dept (page images at HathiTrust; US access only)
• A method for estimating gas turbine-jet airplane performance (Wright Field, Dayton, Ohio : War Department, Army Air Forces, Air Technical Service Command, 1945., 1945), by Robert E. Hage and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Determining operational states of turbojet engines with variable-area tail nozzle (Wright-Patterson Air Force Base, Dayton, Ohio : Headquarters Air Materiel Command, 1948., 1948), by Siegfried H. Hasinger and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Exhaust plume thermodynamic effects on nonaxisymmetric nozzle afterbody performance in transonic flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), by C. E. Robinson, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• An evaluation of jet simulation parameters for nozzle afterbody testing at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by William Lee Peters, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• Investigation of subsonic annular nozzles for engine exhaust/external flow interaction studies (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by R. J. Matz, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
• Evaluation of boattail geometry and exhaust plume temperature effects on nozzle afterbody drag at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1976., 1976), by L. L. Galigher, R. C. Bauer, Steven F. Yaros, Arnold Engineering Development Center, United States. Air Force. Systems Command, and Inc ARO (page images at HathiTrust)
• Introduction to jet engine fundamentals (The Corporation, 1958), by United Aircraft Corporation / Pratt & Whitney Aircraft Division (page images at HathiTrust; US access only)
• Training guide for J73-GE-3, -3A, -3D, turbojet engine (General Electric, Aircraft Gas Turbine Divisions, 1955), by General Electric Company and Aircraft Gas Turbine Training School (page images at HathiTrust; US access only)
• Experimental and analytical determination of integrated airframe nozzle performance. Volume II, Operating manual for twin-nozzle/aftbody drag and internal nozzle performance computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), by Edsel R. Glasgow, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), Lockheed-California Company, and United States. Air Force. Systems Command (page images at HathiTrust)
• Experimental and analytical determination of integrated airframe nozzle performance. Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972, 1972), by Edsel R. Glasgow, S. J. Smyth, R. F. Smith, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), Lockheed-California Company, and United States. Air Force. Systems Command (page images at HathiTrust)

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