Gas-turbines -- Blades -- Cooling -- TestingSee also what's at your library, or elsewhere.
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Filed under: Gas-turbines -- Blades -- Cooling -- Testing
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Filed under: Gas-turbines -- Blades -- Cooling -- CongressesFiled under: Gas-turbines -- Blades -- Cooling -- Equipment and supplies
Filed under: Gas-turbines -- Blades -- Cooling -- Equipment and supplies -- Materials -- OxidationFiled under: Gas-turbines -- Blades -- Cooling -- Equipment and supplies -- Materials -- Thermal propertiesFiled under: Aircraft gas-turbines -- Blades -- Cooling 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) Cold-air annular-cascade investigation of aerodynamic performance of cooled turbine vanes (National Aeronautics and Space Administration ;, 1974), by Louis J. Goldman, Kerry L. McLallin, and Lewis Research Center (page images at HathiTrust) Aerodynamic performance of a ceramic-coated core turbine vane tested with cold air in a two-dimensional cascade (National Aeronautics and Space Administration ;, 1975), by Roy G. Stabe, Curt H. Liebert, 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) Metal temperatures and coolant flow in a wire-cloth transpiration-cooled turbine vane (National Aeronautics and Space Administration ;, 1975), by Herbert J. Gladden (page images at HathiTrust) Turbine vane coolant flow variations and calculated effects on metal temperatures (National Aeronautics and Space Administration ;, 1975), by Frederick C. Yeh, Louis M. Russell, Peter L. Meitner, and Lewis Research Center (page images at HathiTrust) Aerodynamic performance of a fully film cooled core turbine vane tested with cold air in a two-dimensional cascade (National Aeronautics and Space Administration ;, 1975), by Roy G. Stabe, John F. Kline, and Lewis Research Center (page images at HathiTrust) Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), by Charles F. Zalabak, Arthur N. Curren, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Filed under: Aircraft gas-turbines -- Blades -- Cooling -- Mathematical models
Filed under: Gas-turbines -- Cooling -- Testing 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: Gas-turbine disks -- Cooling -- Testing
Filed under: Blades -- Testing Development and testing of a pneumatic scraper blade for conveyor belt cleaning (U.S. Dept. of the Interior, Bureau of Mines, 1989), by C. A. Rhoades, T. L. Hebble, and S. G. Grannes (page images at HathiTrust) Surface pressure measurements at two tips of a model helicopter rotor in hover (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by R. B. Gray, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) Development and testing of a pneumatic scraper blade for conveyor belt cleaning (U.S. Dept. of the Interior, Bureau of Mines, 1989), by C. A. Rhoades, T. L. Hebble, and S. G. Grannes (page images at HathiTrust)
Filed under: Aircraft gas-turbines -- Blades -- Testing 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) Filed under: Airplanes -- Turbojet engines -- Blades -- TestingFiled under: Axial flow compressors -- Blades -- Testing Investigation of an impulse axial-flow compressor rotor over a range of blade angles (National Advisory Committee for Aeronautics, 1950), by Wallace M. Schulze, Willard R. Westphal, John R. Erwin, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) Design, over-all performance and stall characteristics (National Advisory Committee for Aeronautics, 1954), by George W. Lewis, G. K. Serovy, Francis C. Schwenk, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust) Filed under: Compressors -- Blades -- Testing Off-design correlation for losses due to part-span dampers on transonic rotors. (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by William B. Roberts, Donald M. Sandercock, James E. Crouse, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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) Overall and blade element performance of a 1.20-pressure-ratio fan stage with rotor blades reset -5 ̊ (U.S. National Aeronautics and Space Administration ;, 1976), by George W. Lewis, Royce D. Moore, Walter Martin Osborn, and Lewis Research Center (page images at HathiTrust) Overall and blade element performance of a 1.20 pressure ratio fan stage with rotor blades reset -7 ̊ (U.S. National Aeronautics and Space Administration ;, 1976), by George W. Lewis, George Kovich, and Lewis Research Center (page images at HathiTrust) Filed under: Fans (Machinery) -- Blades -- Noise -- TestingFiled under: Gas-turbines -- Blades -- Materials -- Testing An evaluation of three oxidation-resistant alloy claddings for IN 100 and WI 52 superalloys (National Aeronautics and Space Administration ;, 1969), by Michael A. Gedwill, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust) A nickel-base alloy, NASA WAZ-16, with potential for gas turbine stator vane application (National Aeronautics and Space Administration ;, 1974), by William J. Waters, John C. Freche, and Lewis Research Center (page images at HathiTrust) Factors affecting miniature Izod impact strength of tungsten-fiber-metal-matrix composites (National Aeronautics and Space Administration ;, 1973), by Edward A. Winsa, Donald W. Petrasek, and Lewis Research Center (page images at HathiTrust) Stress-rupture strength and microstructural stability of tungsten-hafnium-carbon-wire-reinforced superalloy composites (National Aeronautics and Space Administration ;, 1974), by Donald W. Petrasek, Robert A. Sigorelli, and Lewis Research Center (page images at HathiTrust)
Filed under: Aircraft gas-turbines -- Blades -- Materials -- 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) 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: Turboengines -- Blades -- TestingFiled under: Turbomachines -- Blades -- TestingMore items available under broader and related terms at left. |