Turbines -- Testing -- Data processingSee also what's at your library, or elsewhere.
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Filed under: Turbines -- Testing -- Data processing
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Filed under: Turbines -- Testing- Holyoke hydrodynamic experiments, 1879-80. (Weaver, Shipman and Co., 1880), by Holyoke Water Power Company (page images at HathiTrust)
- Performance evaluation of a two-stage axial-flow turbine for two values of tip clearance (National Aeronautics and Space Administration ;, 1968), by Milton G. Kofskey, William J. Nusbaum, and Lewis Research Center (page images at HathiTrust)
- Experimental evaluation of a 3.50-inch radial turbine designed for a 10-kilowatt space power system (National Aeronautics and Space Administration ;, 1969), by Milton G. Kofskey, Charles A. Wasserbauer, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
- Investigation of a 4.0-inch-mean-diameter four-stage reentry turbine for auxiliary power drives (National Aeronautics and Space Administration, 1960), by Robert Y. Wong, Monroe Daniel E., David L. Darmstadt, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Investigation of transonic turbine designed for zero diffusion of suction-surface velocity (National Advisory Committee for Aeronautics, 1954), by Warren J. Whitney, R. Y. Wong, Daniel E. Monroe, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Experimental investigation of the heat-transfer characteristics of an air-cooled sintered porous turbine blade (National Advisory Committee for Aeronautics, 1952), by Louis J. Jr Schafer, Hadley T. Richards, Edward R. Bartoo, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Determination of blade-to-coolant heat-transfer coefficients on a forced-convection, water-cooled, single-stage turbine (National Advisory Committee for Aeronautics, 1951), by John C. Freche, Eugene F. Schum, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
- Tests of a Spiro turbine (1913), by Arthur Leslie Myers (page images at HathiTrust; US access only)
Filed under: Turbines -- Testing -- PerformanceFiled under: Gas-turbines -- Testing- Bureau of Mines coal-fired gas turbine research project : test of new turbine blade design (U.S. Dept. of the Interior, Bureau of Mines, 1967), by James P. McGee, W. M. Nabors, Donald C. Strimbeck, Robert W. Cargill, Jack Smith, United States Bureau of Mines, and Inc Bituminous Coal Research (page images at HathiTrust)
- Bureau of Mines coal-fired gas turbine research project : test of combustor and ash separators for open-cycle plant (U.S. Dept. of the Interior, Bureau of Mines, 1969), by James P. McGee, Gerald B. Goff, Arthur J. Liberatore, Donald C. Strimbeck, and United States Bureau of Mines (page images at HathiTrust)
- Efficiency of radial-flow turbine of turbo engineering corporation TT13-18 turbo super charger (National Advisory Committee for Aeronautics, 1947), by Earl E. Coulter, William R. Galloway, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
Filed under: Aircraft gas-turbines -- 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)
Filed under: Free piston engines -- Testing
Filed under: Gas-turbines -- Combustion chambers -- Testing- Performance of a vortex-controlled diffuser in an annular swirl-can combustor at inlet Mach numbers up to 0.53 (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979), by John M. Smith (page images at HathiTrust)
- Effect of fuel injector type on performance and emissions of reverse-flow combustor (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981), by Carl T. Norgren and Stephen M. Riddlebaugh (page images at HathiTrust)
- Performance and emission characteristics of swirl-can combustors to a near-stoichiometric fuel-air ratio (National Aeronautics and Space Administration :, 1976), by Larry A. Diehl, Arthur M. Trout, and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Effect of inlet-air humidity, temperature, pressure, and reference Mach number on the formation of oxides of nitrogen in a gas turbine combustor (National Aeronautics and Space Administration ;, 1973), by Nicholas R. Marchionna, Arthur M. Trout, Larry A. Diehl, and Lewis Research Center (page images at HathiTrust)
Filed under: Hydraulic turbines -- Testing- Turbine performance test, Spring Creek Powerplant unit no. 2, Trinity River Division, Central Valley Project : flow measurement by the salt velocity method (United States Department of the Interior, Bureau of Reclamation, 1983), by A. E. Rickett, A. B. Lewey, Central Valley Project (Calif.). Trinity River Division, and United States Bureau of Reclamation (page images at HathiTrust)
- Test of a twelve thousand horse power turbine (1906), by Lucius B. Fuller (page images at HathiTrust; US access only)
- Effect of tip clearance on performance of small axial hydraulic turbine (U.S. National Aeronautics and Space Administration ;, 1976), by James L. Boynton and Harold E. Rohlik (page images at HathiTrust)
Filed under: Steam-turbines -- TestingFiled under: Turbogenerators -- Testing- Turboalternator CSU I-3A (National Aeronautics and Space Administration, 1965), by inc Thompson Ramo Wooldridge and United States National Aeronautics and Space Administration (page images at HathiTrust)
- Computations on the performance of a power station II : nonautomatic extraction turbogenerators (E.I. du Pont de Nemours & Co., Explosives Dept., Atomic Energy Division, Technical Division, Savannah River Laboratory, 1956), by Richard R. Haefner, J. H. Griffin, U.S. Atomic Energy Commission, Savannah River Laboratory, and E.I. du Pont de Nemours & Company (page images at HathiTrust)
Filed under: Turbines -- Aerodynamics -- TestingFiled under: Turbines -- Blades -- Testing- 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)
- Durability of zirconia thermal-barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operation (National Aeronautics and Space Administration ;, 1976), by Lewis Research Center, Curt H. Liebert, and United States National Aeronautics and Space Administration (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)
- Performance evaluation of modified jet-flap rotor blade. (National Aeronautics and Space Administration, 1971), by H. G. Lueders, United States National Aeronautics and Space Administration, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
- Performance evaluation of plain rotor blade with plow type vortex generators (National Aeronautics and Space Administration, 1969), by H. G. Lueders (page images at HathiTrust)
- Experimental investigation of advanced concepts to increase turbine blade loading : II. performance evaluation of plain rotor blade (National Aeronautics and Space Administration, 1968), by H. G. Lueders (page images at HathiTrust; US access only)
- Performance evaluation of jet-flap rotor blade (National Aeronautics and Space Administration, 1970), by H. G. Lueders, United States National Aeronautics and Space Administration, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
- Performance evaluation of modified tandem rotor blade (National Aeronautics and Space Administration, 1970), by H. G. Lueders, United States National Aeronautics and Space Administration, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
- Performance evaluation of a two-stage turbine designed for a ratio of blade speed to jet speed of 0.146 (National Aeronautics and Space Administration, 1960), by Milton G. Kofskey, Lewis Research Center, and United States National Aeronautics and Space Administration (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)
Filed under: Turbines -- Materials -- TestingFiled under: Turbines -- Models -- TestingFiled under: Turbines -- Parts -- TestingMore items available under broader and related terms at left. |