Turbines -- Blades -- CoolingSee also what's at your library, or elsewhere.
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Filed under: Turbines -- Blades -- Cooling Crossflow effects on impingement cooling of a turbine vane (National Aeronautics and Space Administration ;, 1974), by James W. Gauntner and Lewis Research Center (page images at HathiTrust) Effects of film injection angle on turbine vane cooling (National Aeronoautics and Space Administration, Scientific and Technical Information Office ;, 1977), by James W. Guantner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine vane tested with cold air in a two-dimensional cascade (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by John F. Kline, Thomas P. Moffitt, Roy G. Stabe, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) Pressure-loss and flow coefficients inside a chordwise-finned, impingement, convection, and film air-cooled turbine vane (National Aeronautics and Space Administration ;, 1974), by Steven A. Hippensteele and Lewis Research Center (page images at HathiTrust) Heat transfer and pressure drop in blade cooling channels with turbulence promoters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by J. C. Han, C. K. Lei, J. S. Park, Lewis Research Center, and Texas A & M University. Dept. of Mechanical Engineering (page images at HathiTrust) NASA TN D-6065 (National Aeronautics and Space Administration :, 1970), by Marvin E. Goldstein, Robert Siegel, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-5878 (National Aeronautics and Space Administration :, 1970), by Robert Siegel, Marvin E. Goldstein, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) Flow through a wire-form transpiration-cooled vane (National Aeronautics and Space Administration ;, 1973), by Albert Kaufman and Lewis Research Center (page images at HathiTrust) An adverse effect of film cooling on the suction surface of a turbine vane (National Aeronautics and Space Administration ;, 1974), by Herbert J. Gladden, James W. Gauntner, and Lewis Research Center (page images at HathiTrust)
Filed under: Turbines -- Blades -- Cooling -- Congresses
Filed under: Gas-turbines -- Blades -- Cooling -- Congresses
Filed 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: Gas-turbines -- Blades -- Cooling -- TestingFiled 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
Items below (if any) are from related and broader terms.
Filed under: Turbines -- Blades Experimental Boiling Water Reactor turbine blade failure : summary report (Argonne National Laboratory, 1958), by J. M. Harrer, E. A. Wimunc, and Argonne National Laboratory. Reactor Engineering Division (page images at HathiTrust) Aerodynamic pressure and flow-visualization measurement from a rotating wind turbine blade (Solar Energy Research Institute ;, 1989), by C. P. Butterfield, United States. Department of Energy, and Solar Energy Research Institute (page images at HathiTrust; US access only) Prediction method for two-dimensional aerodynamic losses of cooled vanes using integral boundary-layer parameters (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Louis J. Goldman, Raymond E. Gaugler, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust) Computer program for generating input for analysis of impingement-cooled, axial-flow turbine blade (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by David Rosenbaum, Lewis Research Center, Army Research and Technology Laboratories (U.S.). Structures Laboratory, Propulsion Laboratory (U.S.), and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust) NASA TM X-3045 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1974), by Thomas P. Moffitt, Wayne M. Bartlett, Herman W. Prust, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust) Two-dimensional cold-air cascade study of a film-cooled turbine stator blade : IV, comparison of experimental and analyatical aerodynamic results for blade with 12 rows of 0.076-centimeter (0.030-in.-) diameter holes having streamwise ejection angles (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Herman W. Prust, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) Method for calculating convective heat-transfer coeffecients over turbine vane surfaces (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Daniel J. Gauntner, James Sucec, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust) Cold-air annular-cascade investigation of aerodynamic performance of core-engine-cooled turbine vanes : II--Pressure surface trailing edge ejection and split trailing edge ejection (U.S. National Aeronautics and Space Administration ;, 1976), by Kerry L. McLallin, Louis J. Goldman, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust) Surface pyrometry in presence of radiation from other sources with application to turbine-blade temperature measurement (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Donald R. Buchele, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust) Experimental investigation of advanced concepts to increase turbine blade loading. III, Performance evaluation of tandem rotor blade (National Aeronautics and Space Administration ;, 1968), by H. G. Lueders, General Motors Corporation. Allison Division, and Lewis Research Center (page images at HathiTrust) Three-stage potassium turbine performance test summary (National Aeronautics and Space Administration ;, 1969), by G. C. Wesling, Lewis Research Center, and General Electric Company (page images at HathiTrust) Oxidation resistant porous material for transpiration cooled vanes (National Aeronautics and Space Administration ;, 1972), by P. Madsen, Robert M. Rusnak, Lewis Research Center, and Bendix Corporation (page images at HathiTrust) Dynamic response of high-frequency pressure transducers to large amplitude sinusoidal pressure oscillations (National Aeronautics and Space Administration ;, 1972), by Richard E. Robinson, Lewis Research Center, and Battelle Memorial Institute (page images at HathiTrust) An experimental study of near wall flow parameters in the blade end-wall corner region (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), by Rakesh K. Bhargava, Rishi S. Raj, and Lewis Research Center (page images at HathiTrust) NASA TN D-5282 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Albert Kaufman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust) NASA TN D-5855 (National Aeronautics and Space Administration ;, 1970), by Royce D. Moore, Phillip R. Meng, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only) Experimental results of varying the blade-shroud clearance in a 6.02-inch radial-inflow turbine (National Aeronautics and Space Administration ;, 1970), by Samuel M. Futral and Donald E. Holeski (page images at HathiTrust) Alkali-metal turbine geometry affected by blade-speed limitations (National Aeronautics and Space Administration ;, 1965), by Arthur J. Glassman and Lewis Research Center (page images at HathiTrust) Miniature sheathed thermocouples for turbine blade temperature measurement (National Aeronautics and Space Administration ;, 1974), by Raymond Holanda, Lloyd N. Krause, George E. Glawe, and Lewis Research Center (page images at HathiTrust) Effect of chord size on weight and cooling characteristics of air-cooled turbine blades (National Advisory Committee for Aeronautics, 1957), by Jack B. Esgar, Arthur N. Curren, Eugene F. Schum, and United States National Advisory Committee for Aeronautics (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, 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. Schafer, Hadley T. Richards, Edward R. Bartoo, 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, 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, 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, and Lewis Flight Propulsion Laboratory (page images at HathiTrust) Analytical investigation of two liquid cooling systems for turbine blades (National Advisory Committee for Aeronautics, 1951), by Thomas W. Jackson, John N. B. Livingood, and Lewis Flight Propulsion Laboratory (page images at HathiTrust) Blade-to-coolant heat-transfer results and operating data from a natural-convection water-cooled single-stage turbine (National Advisory Committee for Aeronautics, 1951), by Anthony J. Diaguila, John C. Freche, 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, 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, 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, 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) Preliminary investigation of hollow-bladed turbines having closed and open blade tips (National Advisory Committee for Aeronautics, 1955), by Gordon T. Smith, Robert O. Hickel, 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) Effect of centrifugal force on flutter of uniform cantilever beam at subsonic speeds with application to compressor and turbine blades (National Advisory Committee for Aeronautics, 1949), by Alexander Mendelson and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Effects of some solution treatments followed by an aging treatment on the life of small cast gas-turbine blades of a cobalt-chromium-base alloy. [Part] 1, Effect of solution-treating temperature (National Advisory Committee for Aeronautics, 1951), by C. Yaker, C. A. Hoffman, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Analysis of temperature distribution in liquid-cooled turbine blades (National Advisory Committee for Aeronautics, 1951), by John N. B. Livingood, W. Byron Brown, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Experimental investigation of loss in an annular cascade of turbine-nozzle blades of free vortex design (National Advisory Committee for Aeronautics, 1953), by Hubert W. Allen, Richard E. Chamness, Milton G. Kofskey, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Study of secondary-flow patterns in an annular cascade of turbine nozzle blades with vortex design (National Advisory Committee for Aeronautics, 1953), by Harold E. Rohlik, Howard Z. Herzig, Hubert W. Allen, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles (National Advisory Committee for Aeronautics, 1953), by Milton G. Kofskey, Howard Z. Herzig, Hubert W. Allen, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades (National Advisory Committee for Aeronautics, 1951), by William R. Slivka, David H. Silvern, Lewis Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) Design and experimental investigation of two rotor blade modifications for a high-weight-flow low-pressure-ratio turbine (National Aeronautics and Space Administration, 1959), by Robert R. Nunamaker, Charles A. Wasserbauer, Donald A. Petrash, and United States National Aeronautics and Space Administration (page images at HathiTrust) Exact analytical solution to a transient conjugate heat-transfer problem (National Aeronautics and Space Administration ;, 1973), by James Sucec and Lewis Research Center (page images at HathiTrust) Program to develop a wrought blade superalloy (General Electric, Nuclear Materials and Propulsion Operation, 1961), by Wilford H. Couts, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust) NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by Ernest R. Chanes, L. Robert Carman, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust) The mutual interference of rows of blades of axial flow pumps, fans and turbines (1938), by Finn Jonassen (page images at HathiTrust) Theoretical and experimental cascade flow investigations at high subsonic Mach numbers ([Washington, D.C.] : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1959., 1959), by U. Hopkes and United States. Air Force. Office of Scientific Research (page images at HathiTrust) Research on exploratory development of nondestructive methods for crack detection : Part IV (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by Rudi Schroeer, Partha Sirkar, Frank O'Keefe, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust) Eddy current inspection of turbine blades (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by I. R. Kraska, H. W. Kamm, Air Force Materials Laboratory (U.S.), and General American Transportation Corporation (page images at HathiTrust)
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