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Automotive gas turbines -- Cooling

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• Automotive gas turbines
• Automobiles -- Motors -- Cooling
• Gas-turbines -- Cooling
• Cooling

• Air cooling of disk of a solid integrally cast turbine rotor for an automotive gas turbine (National Aeronautics and Space Administration ;, 1977), by Herbert J. Gladden (page images at HathiTrust)

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

• Cold-air performance of compressor-drive turbine of Department of Energy upgraded automobile gas turbine engine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Richard J. Roelke, Jeffrey E. Haas, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Propulsion Laboratory (U.S.), and Lewis Research Center (page images at HathiTrust)
• Cold-air performance of a 15.41-cm-tip-diameter axial-flow power turbine with variable-area stator designed for a 75-kW automotive gas turbine engine (National Aeronautics and Space Administration ;, 1982), by Kerry L. McLallin, Robert Y. Wong, Milton G. Kofskey, United States. Dept. of Energy. Office of Vehicle and Engine Research and Development, and Lewis Research Center (page images at HathiTrust)
• Cold-air performance of free-power turbine designed for 112-kilowatt automotive gas-turbine engine : I - Design stator-vane-chord setting angle of 35 ̊ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Milton G. Kofskey, William J. Nusbaum, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• High temperature self-lubricating coatings for air lubricated foil bearings for the automotive gas turbine engine (Dept. of Energy, Transportation Energy Conservation Division ;, 1980), by Bharat Bhushan, United States. Department of Energy. Division of Transportation Energy Conservation, Lewis Research Center, and Mechanical Technology Incorporated (page images at HathiTrust)

• Multiroller traction drive speed reducer : evaluation for automotive gas turbine engine (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Douglas A. Rohn, Neil E. Anderson, Stuart H. Loewenthal, Army Research and Technology Laboratories (U.S.), United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Propulsion Laboratory (U.S.), and Lewis Research Center (page images at HathiTrust)

• Cold-air study of the effect on turbine stator blade aerodynamic performance of coolant ejection from various trailing-edge slot geometries (National Aeronautics and Space Administration ;, 1974), by Herman W. Prust, Wayne M. Bartlett, and Lewis Research Center (page images at HathiTrust)
• Film cooling on the pressure surface of a turbine vane (National Aeronautics and Space Administration ;, 1977), by James W. Gauntner, Herbert J. Gladden, and United States National Aeronautics and Space Administration (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)
• Streakline flow visualization of discrete-hole film cooling with normal, slanted and compound angle injection (National Aeronautics and Space Administration ;, 1976), by Raymond S. Colladay, Louis M. Russell, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Coolant pressure and airflow distribution in a strut-supported transpiration-cooled vane for a gas turbine engine (National Aeronautics and Space Administration ;, 1972), by Albert Kaufman, Hadley T. Richards, David J. Poferl, United States National Aeronautics and Space Administration, and Lewis Research Center (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, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• A summary of design information for water-cooled turbines (National Advisory Committee for Aeronautics, 1951), by John C. Freche, United States National Advisory Committee for Aeronautics, 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, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Determination of gas-to-blade convection heat-transfer coefficients on a forced-convection, water-cooled single-stage aluminum 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)
• Cooling of gas turbines [Part] 2, effectiveness of rim cooling of blades (National Advisory Committee for Aeronautics, 1947), by L. Wolfenstein, John S. McCarthy, Gene L. Meyer, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• Cooling of gas turbines [Part] 4, Calculated temperature distribution in the trailing part of a turbine blade using direct liquid cooling (National Advisory Committee for Aeronautics, 1947), by W. Byron Brown, William R. Monroe, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• Cooling of gas turbines [Part] 8, Theoretical temperature distributions through gas turbine with special blades and cooling fins on the rim (National Advisory Committee for Aeronautics, 1948), by W. Byron Brown, John N. B. Livingood, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Cooling of gas turbines [Part] 5, Effectiveness of air cooling of hollow blades (National Advisory Committee for Aeronautics, 1947), by L. Wolfenstein, John S. McCarthy, Robert L. Maxwell, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• Cooling of gas turbines [Part] 3, Analysis of rotor and blade temperatures in liquid-cooled gas turbines (National Advisory Committee for Aeronautics, 1947), by W. Byron Brown, John N. B. Livingood, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)

• NACA Conference on Turbine Cooling : a compilation of the papers presented by NACA staff members, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, November 9, 1949 (NACA, 1949), by Ohio) NACA Conference on Turbine Cooling (1949 : Cleveland, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• NACA Conference on Turbine Materials and Cooling : a compilation of the papers presented, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, March 15, 1951 (NACA, 1951), by Ohio) NACA Conference on Turbine Materials and Cooling (1951 : Cleveland, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• NACA Conference on Turbine Materials and Cooling : a compilation of the papers presented, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, March 15, 1951 (NACA, 1951), by Ohio) NACA Conference on Turbine Materials and Cooling (1951 : Cleveland, Lewis Flight Propulsion Laboratory, and United States National Advisory Committee for Aeronautics (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)

• Evaluation of a compressor bleed system for rim cooling the turbine wheel of a turbojet engine (National Advisory Committee for Aeronautics, 1954), by C. R. Morse, R. H. Kemp, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• Stagnation region gas film cooling : spanwise angled injection from multiple rows of holes (National Aeronautics and Space Administration ;, 1981), by D. W. Luckey, M. R. L'Ecuyer, Lewis Research Center, Purdue University. Thermal Sciences and Propulsion Center, United States National Aeronautics and Space Administration, and United States. Office of Naval Research (page images at HathiTrust)

• Extension of similarity test procedures to cooled engine components with insulating ceramic coatings (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Herbert J. Gladden, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

• An analysis of the capabilities and limitations of turbine air cooling methods (National Aeronautics and Space Administration ;, 1970), by Jack B. Esgar, Albert Kaufman, Raymond S. Colladay, and Lewis Research Center (page images at HathiTrust)

• An analysis of the capabilities and limitations of turbine air cooling methods (National Aeronautics and Space Administration ;, 1970), by Jack B. Esgar, Albert Kaufman, Raymond S. Colladay, and Lewis Research Center (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)
• 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)

• Measurements of liner cooling effectiveness within a full-scale double-annular ram-induction combustor (National Aeronautics and Space Administration ;, 1974), by Edward J. Mularz, Donald F. Schultz, and U.S. Army Air Mobility Research and Development Laboratory (page images at HathiTrust)

• Flow measurement in base cooling air passages of a rotating turbine blade (National Aeronautics and Space Administration ;, 1974), by Curt H. Liebert, Frank G. Pollack, and Lewis Research Center (page images at HathiTrust)

• Effect of free-stream turbulence on film cooling (National Aeronautics and Space Administration ;, 1975), by Cecil J. Marek, Robert R. Tacina, and Lewis Research Center (page images at HathiTrust)
• Film cooling in a combustor operating at fuel-rich exit conditions (National Aeronautics and Space Administration ;, 1974), by Robert R. Tacina, Cecil J. Marek, and Lewis Research Center (page images at HathiTrust)

• The quenching of steels (American Society for Steel Treating, 1930), by Herbert J. French (page images at HathiTrust)
• On methods of obtaining cooling curves (Govt. print. off., 1908), by G. K. Burgess and United States. Bureau of Standards (page images at HathiTrust)
• Tests of a heat pump for domestic heating and cooling / by E.P. Carman. (U.S. Dept. of the Interior, Bureau of Mines, 1953), by E. P. Carman (page images at HathiTrust)
• Recent developments in spray cooling of deep mines (U.S. Dept. of the Interior, Bureau of Mines, 1986), by Edward D. Thimons, John R. Marks, and John F. McCoy (page images at HathiTrust)
• Cooling mine air during summer months to prevent roof falls (Dept. of the Interior, Bureau of Mines, 1940), by C. A. Herbert and United States Bureau of Mines (page images at HathiTrust)
• Cooling of mine air (U.S. Dept. of the Interior, Bureau of Mines, 1923), by Thomas Thornton Read, F. C. Houghten, and United States Bureau of Mines (page images at HathiTrust)
• Cooling methods for electronic equipment (U.S. Govt. Print. Off, 1955), by United States Navy Department Bureau of Ships (page images at HathiTrust)
• Analysis of uncertainities in turbine metal temperature predictions (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Francis S. Stepka and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerothermal performance of a radiatively and actively cooled panel at Mach 6.6 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Charles P. Shore, Irving Weinstein, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Effects of mass addition on blunt-body boundary-layer transition and heat transfer (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by George E. Kaattari and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Vortex-generating coolant-flow-passage design for increased film-cooling effectiveness and surface coverage (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by S. Stephen Papell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Film-cooling effectiveness with developing coolant flow through straight and curved tubular passages (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by S. Stephen Papell, Robert W. Graham, Chi R. Wang, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A feasibility study of heat-pipe-cooled leading edges for hypersonic cruise aircraft (National Aeronautics and Space Administration, 1971), by Calvin C. Silverstein, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Automatic control of water cooling in space suits (National Aeronautics and Space Administration, 1968), by Paul Webb, Samuel J. Troutman, and James F. Annis (page images at HathiTrust; US access only)
• An analytical study of hydrogen cooled panels for application to hypersonic aircraft (National Aeronautics and Space Administrtion, 1971), by W. G. Flieder, Langley Research Center, Garrett Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6152 (National Aeronautics and Space Administration ;, 1971), by Alden F. Presler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analysis of heat transfer in a porous cooled wall with variable pressure and temperature along the coolant exit boundary (National Aeronautics and Space Administration ;, 1972), by Robert Siegel, Marvin E. Goldstein, and Lewis Research Center (page images at HathiTrust)
• Analysis and comparison of wall cooling schemes for advanced gas turbine applications (National Aeronautics and Space Administration, 1972), by Raymond S. Colladay, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Crash-fire protection system for a J57 turbojet engine using water as a cooling and inerting agent (National Aeronautics and Space Administration, 1960), by Dugald O. Black and Lewis Research Center (page images at HathiTrust)
• Analysis of shape of porous cooled medium for an imposed surface heat flux and temperature (National Aeronautics and Space Administration ;, 1973), by Robert Siegel and Lewis Research Center (page images at HathiTrust)
• An integral analysis of heat transfer downstream of a rearward-facing step with small coolant injection. (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Keiichi Karashima (page images at HathiTrust; US access only)
• 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)
• Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), by Arthur N. Curren, Charles F. Zalabak, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, 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)
• Investigation of 75-millimeter-bore cylindrical-roller bearings at high speeds. [Part] III, Lubrication and cooling studies - oil inlet distribution, oil inlet temperature, and generalized single-oil-jet cooling-correlation analysis (National Advisory Committee for Aeronautics, 1951), by E. Fred Macks, Zolton N. Nemeth, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• The compressible laminar boundary layer with fluid injection (National Advisory Committee for Aeronautics, 1955), by George M. Low and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Experimental data on stagnation-point gas injection cooling on a hemisphere-cone in a hypersonic arc tunnel (National Aeronautics and Space Administration ;, 1964), by John E. Grimaud, Leonard C. McRee, and Langley Research Center (page images at HathiTrust)
• Organic coolant impurities removal (Atomics International, 1962), by G. O. Haroldsen, H. Powell, G. Garabedian, G. Berg, J. W. Florence, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Coolant decomposition rates and makeup costs for organic reactors (Canoga Park, California : Atomics International, 1964., 1964), by R. H. J. Gercke, J. F. Zack, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Comparative effectiveness of a convection-type and a radiation-type cooling cap on a turbosupercharger (National Advisory Committee for Aeronautics ;, 1946), by Frederick J. Hartwig and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Feasibility study of water-cooled thermionic nuclear power plant. (Office of Technical Services, Dept. of Commerce, 1962), by Martin Company, U.S. Atomic Energy Commission, Martin Company. Nuclear Division, and N.G. Asbed (page images at HathiTrust)
• Extreme temperature range organic coolants. (Wright Air Development Division, Air Research and Development Command, U. S. Air Force, 1961), by Dale A. Barsness (page images at HathiTrust)
• Cooling and air conditioning for comfort; theory and calculations (The Aerologist Pub. Co., 1932), by William Goodman (page images at HathiTrust; US access only)
• The use of reservoirs and lakes for the dissipation of heat. (Washington, 1953), by Guy Earl Harbeck (page images at HathiTrust)
• Transpiration cooling experiments near the stagnation line of a cylinder in cross flow (White Oak, Maryland : United States Naval Ordnance Laboratory, 1970., 1970), by Richard L. Humphrey and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Intermittent service, iced ventilating system (University of Texas, 1948), by James Dorr McFarland, Willis Raymond Woolrich, and Harold A. Tankersley (page images at HathiTrust; US access only)
• Transient behavior of a natural-circulation loop operating near the thermodynamic critical point (Argonne National Laboratory, Reactor Engineering Division, 1963), by Darrel G. Harden and Argonne National Laboratory (page images at HathiTrust)
• Subsurface, surface, and boundary layer interactions of various transpirants with carbon (Albuquerque, New Mexico : Sandia Corporation, 1971., 1971), by Thomas J. Dahm, U.S. Atomic Energy Commission, Aerotherm Corporation, and Sandia Corporation (page images at HathiTrust)
• Cooldown of cryogenic transfer lines (Los Alamos, New Mexico : Los Alamos Scientific Laboratory of the University of California, 1965., 1965), by D. H. Liebenberg, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Operating experience with the sodium reactor experiment and its application to the Hallam nuclear power facility (Oak Ridge, Tennessee : USAEC Division of Technical Information Extension, 1961., 1961), by R. J. Beeley, J. E. Mahlmeister, U.S. Atomic Energy Commission. Technical Information Center, and North American Aviation. Atomics International Division (page images at HathiTrust)
• Extending human tolerance to heat by prior body cooling (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by James H. Veghte, Paul Webb, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
• Resonant jets for turbine cooling (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1991., 1991), by M. Kurosaka, University of Washington. Department of Aeronautics and Astronautics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• A combined experimental/computational study of flow in turbine blade cooling passage (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1994), by D. G. N. Tse, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, and Lewis Research Center (page images at HathiTrust)

More items available under broader and related terms at left.