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Aircraft gas-turbines -- Testing

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• Aircraft gas-turbines
• Gas-turbines -- Testing
• Testing

• Aircraft gas-turbines -- Testing -- Equipment and supplies
• Aircraft gas-turbines -- Blades -- Testing
• Aircraft gas-turbines -- Combustion chambers -- Testing
• Aircraft gas-turbines -- Materials -- Testing

• Preliminary study of methods for providing thermal shock resistance to plasma-sprayed ceramic gas-path seals (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by Robert C. Bill, David E. Brewe, and Donald W. Wisander (page images at HathiTrust)
• 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)
• Experimental flow coefficients of a full-coverage film-cooled-vane chamber (National Aeronautics and Space Administration., 1977), by Peter L. Meitner, Steven A. Hippensteele, U.S. Army Air Mobility Research and Development Laboratory, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effect of primary zone equivalence ratio on pollutant formation (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Russell W. Claus, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Research turbine for high-temperature core engine application (National Aeronautics and Space Administration ;, 1974), by Edward M. Szanca and Lewis Research Center (page images at HathiTrust)
• Spin synchronous X-ray sinography (SXS) for nondestructive imaging of turbine engines under loads (Federal Aviation Administration, Office of Aviation Research ;, 1996), by T. Kirchener, J. Youngberg, P. Burnstein, Foster-Miller, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Turbine engine diagnostics system study (FAA Technical Center ;, 1991), by Barbara K. McQuiston, Ronald L. De Hoff, Inc Systems Control Technology, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)

• Integrated exhaust gas analysis system for aircraft turbine engine component testing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Robert L. Summers, Robert C. Anderson, and Lewis Research Center (page images at HathiTrust)

• Effect of hole geometry and electric-discharge machining (EDM) on airflow rates through small-diameter holes in turbine-blade material (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980), by Steven A. Hippensteele and Reeves P. Cochran (page images at HathiTrust)
• Flow visualization of discrete-hole film cooling with a spanwise injection over a cylinder (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Louis M. Russell, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Gas turbine ceramic-coated-vane concept with convection-cooled porus metal core (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Albert F. Kascak, Lewis Research Center, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Turbine engine diagnostics system study (FAA Technical Center ;, 1991), by Barbara K. McQuiston, Ronald L. De Hoff, Inc Systems Control Technology, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)

• Effect of fiber diameter and matrix alloys on impact-resistant boron/aluminum composites (National Aeronautics and Space Administration :, 1976), by David L. McDanels, Robert A. Signorelli, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Directionally solidified iron-base eutectic alloys (National Aeronautics and Space Administration ;, 1976), by Surendra N. Tewari and United States National Aeronautics and Space Administration (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)

• Effect of exposure cycle on hot-salt stress-corrosion of a titanium alloy (National Aeronautics and Space Administration ;, 1974), by Hugh R. Gray, James R. Johnston, and Lewis Research Center (page images at HathiTrust)
• Resistance of a [gamma]/[gamma]-́[delta] directionally solidified eutectic alloy to recrystallization (National Aeronautics and Space Administration ;, 1975), by Surendra N. Tewari, Charles W. Andrews, Coulson M. Scheuermann, and Lewis Research Center (page images at HathiTrust)
• Effects of carbon and hafnium concentrations in wrought powder-metallurgy superalloys based on NASA IIB-11 alloy (National Aeronautics and Space Administration ;, 1976), by Robert V. Miner and Lewis Research Center (page images at HathiTrust)
• Experimental evaluation of the series-hybrid rolling-element bearing (National Aeronautics and Space Administration ;, 1970), by Richard J. Parker and Lewis Research Center (page images at HathiTrust)
• Effect of chlorine purification on oxidation resistance of some mechanical carbons (National Aeronautics and Space Administration ;, 1974), by Donald W. Wisander, Gordon P. Allen, and Lewis Research Center (page images at HathiTrust)

• Hot-salt stress-corrosion of a titanium alloy under a simulated turbine-engine compressor environment (National Aeronautics and Space Administration ;, 1969), by Hugh R. Gray, James R. Johnston, and Lewis Research Center (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)

More items available under broader and related terms at left.