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Aircraft gas-turbines -- Data processing

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• Aircraft gas-turbines
• Data processing

• Nonlinear, three-dimensional finite-element analysis of air-cooled gas turbine blades (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Albert Kaufman, Raymond E. Gaugler, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

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

• The Aerothermodynamics of aircraft gas turbine engines (Air Force Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command ;, 1978), by Gordon C. Oates, Air Force Aero Propulsion Laboratory (U.S.), and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Turbine design and application (Scientific and Technical Information Office, National Aeronautics and and Space Administration: [For sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1972), by Arthur J. Glassman (page images at HathiTrust; US access only)
• Programmed text : T-53-L-13 gas turbine engine. (U.S. Army Aviation Center, 1985), by U.S. Army Aviation Center (page images at HathiTrust)
• On friction and leakage losses in the working blade-rings of radial flow turbines in helicopter and transport gas-turbine units (National Aeronautics and Space Administration, 1967), by N. F. Galit︠s︡kiĭ (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)
• FORTRAN program to generate engine inlet flow contour maps and distortion parameters (National Aeronautics and Space Administration ;, 1974), by John H. Dicus and Lewis Research Center (page images at HathiTrust)
• Effect of casing treatment on overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5 (National Aeronautics and Space Administration ;, 1977), by Walter M. Osborn, Royce D. Moore, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of swirler-mounted mixing venturi on emissions of flame-tube combustor using Jet A fuel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by David B. Ercegovic, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Emittance and absorptance of NASA ceramic thermal barrier coating system (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Curt H. Liebert and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Two-layer thermal barrier coating for turbane airfoils - furnace and burner rig test results (U.S. National Aeronautics and Space Administration ;, 1976), by Stephan Stecura, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Evaluation of drilled-ball bearings at DN values to three million (National Aeronautics and Space Administration ;, 1972), by P. W. Holmes, Lewis Research Center, and United Aircraft Corporation. Pratt & Whitney Aircraft Division (page images at HathiTrust)
• Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by L. W. Florschuetz, C. R. Truman, Darryl E. Metzger, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• NASA TN D-6702 (National Aeronautics and Space Administration :, 1972), by Arthur J. Glassman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Computer program for quasi-one-dimensional compressible flow with area change and friction : application to gas film seals (National Aeronautics and Space Administration ;, 1974), by John Zuk, Patricia J. Smith, and Lewis Research Center (page images at HathiTrust)
• Similarity constraints in testing of cooled engine parts (National Aeronautics and Space Administration ;, 1974), by Raymond S. Colladay, Francis S. Stepka, and Lewis Research Center (page images at HathiTrust)
• Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), by William A. Fleming, Robert O. Jr Dietz, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800 degrees R (National Advisory Committee for Aeronautics, 1948), by Robert C. Kohl, Robert G. Larkin, 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)
• Analysis of turbine performance of 19B-8 engine (National Advisory Committee for Aeronautics, 1948), by Richard P. Krebs, Frank L. Suozzi, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Analysis of compressor performance (National Advisory Committee for Aeronautics, 1948), by Robert O. Dietz, John K. Kuenzig, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades (National Advisory Committee for Aeronautics, 1948), by John C. Freche, Bob W. Sheflin, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Evaluation of lightweight material concepts for aircraft turbine engine rotor failure protection (Federal Aviation Administration, Office of Aviation Research ;, 1997), by Dy D. Le, U.S. Army Research Laboratory, Naval Air Warfare Center (U.S.). Aircraft Division, Federal Aviation Administration Technical Center (U.S.), and United States. Office of Aviation Research (page images at HathiTrust)
• Statistics on aircraft gas turbine engine rotor failures that occurred in U.S. commercial aviation during 1986 (Federal Aviation Administration Technical Center ;, 1990), by R. A. DeLucia, B. C. Fenton, J. T. Salvino, Naval Air Propulsion Test Center, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Statistics on aircraft gas turbine engine rotor failures that occurred in U.S. commercial aviation during 1988 (Federal Aviation Administration Technical Center ;, 1992), by R. A. DeLucia, E. R. Chapdelaine, B. C. Fenton, Naval Air Propulsion Test Center, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• A dynamic performance computer for gas turbine engines (Wright-Patterson Air Force Base, Ohio : Power Plant Laboratory, Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by V. L. Larrowe, M. M. Spencer, Wright Air Development Center, University of Michigan, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• 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)
• 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)

• Preparation and handling of magnesium-hydrocarbon slurries for jet-engine applications (National Advisory Committee for Aeronautics, 1955), by Henry C. Barnett, Paul H. Wise, Albert M. Lord, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)

• On friction and leakage losses in the working blade-rings of radial flow turbines in helicopter and transport gas-turbine units (National Aeronautics and Space Administration, 1967), by N. F. Galit︠s︡kiĭ (page images at HathiTrust)
• Incidence loss for a core turbine rotor blade in a two-dimensional cascade (National Aeronautics and Space Administration ;, 1974), by Roy G. Stabe, John F. Kline, and Lewis Research Center (page images at HathiTrust)
• Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Kerry L. McLallin, Jeffrey E. Haas, Propulsion Laboratory (U.S.), Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effect of rotor-to-stator spacing on acoustic performance of a full-scale fan (QF-5) for turbofan engines (National Aeronautics and Space Administration ;, 1974), by Joseph R. Balombin, Edward G. Stakolich, and Lewis Research Center (page images at HathiTrust)
• Thermal stress analysis of ceramic gas-path seal components for aircraft turbines (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Francis E. Kennedy, Robert C. Bill, Lewis Research Center, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Reaction diffusion in the nickel-chromium-aluminum and cobalt-chromium-aluminum systems (National Aeronautics and Space Administration ;, 1977), by Stanley R. Levine and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Procedure for calculating turbine blade temperatures and comparison of calculated with observed values for two stationary air-cooled blades (NACA, 1952), by W. Byron Brown, Hadley T. Richards, Henry O. Slone, United States National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
• Effect of high rotor pressure-surface diffusion on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1955), by James W. Miser, Daniel E. Monroe, Warner L. Stewart, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Effect of a reduction in stator solidity on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1956), by James W. Miser, R. Y. Wong, Warner L. Stewart, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine (National Advisory Committee for Aeronautics, 1957), by Cavour H. Hauser, William J. Nusbaum, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Cascade investigation of cooling characteristics of a corrugated-insert air-cooled turbine blade for use in a turboprop engine (National Aeronautics and Space Administration, 1960), by Hadley T. Richards and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Fiber reinforced structures for small turbine engine fragment containment (Phase II). (Federal Aviation Administration, Office of Aviation Research ;, 1996), by Inc Pepin Associates and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)

• Use of fluidic oscillator to measure fuel-air ratios of combustion gases (National Aeronautics and Space Administration ;, 1974), by Stephen M. Riddlebaugh and Lewis Research Center (page images at HathiTrust)
• Effect of exhaust gas recirculation on emissions from a flame-tube combustor using liquid Jet A Fuel (National Aeronautics and Space Administration ;, 1976), by Cecil J. Marek, Robert R. Tacina, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Emissions of oxides of nitrogen from an experimental premixed-hydrogen burner (U.S. National Aeronautics and Space Administration ;, 1976), by David N. Anderson, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effect of premixing quality on oxides of nitrogen in gas turbine combustors (National Aeronautics and Space Administration ;, 1976), by Gerald Roffe, Antonio Ferri, Lewis Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Pollutant formation in fuel lean reciruclating flows (National Aeronautics and Space Administration ;, 1976), by Robert W. Schefer, R. F. Sawyer, Berkeley University of California, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of the effect of cycle pressure on lean combustion emission (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Gerald Roffe, K. S. Venkataramani, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• High-pressure flame system for pollution studies with results for methane-air diffusion flames (National Aeronautics and Space Administration ;, 1977), by Irvin M. Miller, Howard G. Maahs, and United States National Aeronautics and Space Administration (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) (National Aeronautics and Space Administration ;, 1973), by J. Robert Branstetter, Gregory M. Reck, and Lewis Research Center (page images at HathiTrust)
• Carbon-deposition characteristics of MIL-F-5624A fuels containing high-boiling aromatic hydrocarbons (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)
• Numerical modelling of ramjet combustors (Wright-Patterson Air Force Base, Ohio : Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Warren H. Harch and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)

More items available under broader and related terms at left.