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Pump turbines -- Testing

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• Pump turbines
• Hydraulic turbines -- Testing
• Pumping machinery -- Testing
• Turbomachines -- Testing
• Testing

• NASA TN D-4392 (National Aeronautics and Space Administration ;, 1968), by Roy G. Stabe, John F. Kline, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

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

• NASA TN D-4387 (National Aeronautics and Space Administration ;, 1968), by Royce D. Moore, Robert S. Ruggeri, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• NASA TN D-4392 (National Aeronautics and Space Administration ;, 1968), by Roy G. Stabe, John F. Kline, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Proportions of elbow-type suction tubes for large pumps. (U.S. Dept. of the Interior, Bureau of Reclamation, Division of Design, Hydraulic Machinery Branch, 1964), by United States. Bureau of Reclamation. Hydraulic Machinery Branch (page images at HathiTrust)

• Analysis of environmental issues related to small-scale hydroelectric development, IV : fish mortality resulting from turbine passage (Oak Ridge National Laboratory ;, 1981), by Susan C. Turbak, Carole R. Shriner, Donna R. Reichle, and Oak Ridge National Laboratory. Environmental Sciences Division (page images at HathiTrust)

• NASA TN D-4392 (National Aeronautics and Space Administration ;, 1968), by Roy G. Stabe, John F. Kline, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Pump-turbine performance test : Mt. Elbert Pumped-Storage Powerplant and Forebay Dam, Unit 1, Fryingpan-Arkansas Project, Colorado : flow measurement by the salt velocity method. (U.S. Dept. of Interior, Bureau of Reclamation ;, 1984), by United States Bureau of Reclamation (page images at HathiTrust)

• 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)

• Maximum volume-to-stress ratio for a two-radii-contour diaphragm pump (Oak Ridge National Laboratory, 1960), by R. D. Cheverton, U.S. Atomic Energy Commission, Union Carbide Corporation, and Oak Ridge National Laboratory. Reactor Experimental Engineering Division (page images at HathiTrust)
• NASA TN D-5225 (National Aeronautics and Space Administration ;, 1969), by Lawrence P. Ludwig, Robert L. Johnson, Thomas N. Strom, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6543 (National Aeronautics and Space Administration :, 1971), by William Stevans, Robert J. Blade, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Molten Plutonium Pump Experiment (Los Alamos Scientific Laboratory of the University of California, 1962), by John E. Deverall, G. L. Caldwell, Los Alamos Scientific Laboratory. K- Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Dut trial of a 40,000,000-gallon duplex triple expansion Worthington pumping engine (1909), by Eugene Campbell McMillan (page images at HathiTrust; US access only)
• Loss of head in pump valves (1907), by William Emery Brewer (page images at HathiTrust; US access only)
• Loss of head in pump valves (1908), by Theron Robinson Howser (page images at HathiTrust; US access only)
• Relation of speed of centrifugal pumps to height of lift (1906), by Edward J. Mehren (page images at HathiTrust; US access only)
• A study of water rates of prime movers (1913), by Lewis Brown Ermeling (page images at HathiTrust; US access only)
• Test of a De Laval turbo-pump (1906), by Alfred Rittscher Bench and Louis Paul Robert (page images at HathiTrust; US access only)
• Tests of the pumps and wells of the University of Illinois (1914), by John Edwin Lewis and Raymond Thomas Reilly (page images at HathiTrust; US access only)
• The use of compressed air for pumping water (1900), by George Russell Smith (page images at HathiTrust; US access only)
• Selected methods for pumping test analysis (Illinois State Water Survey, 1955), by Jack Bruin, H. E. Hudson, and Illinois State Water Survey (page images at HathiTrust; US access only)
• Selected methods for pumping test analysis (Illinois State Water Survey, 1961), by Jack Bruin, H. E. Hudson, and Illinois State Water Survey (page images at HathiTrust; US access only)

• Factors affecting capacity of air lifts (Idaho Operations Office, U.S. Atomic Energy Commission, 1957), by H. V. Chamberlain, Phillips Petroleum Company. Atomic Energy Division, and U.S. Atomic Energy Commission. Idaho Operations Office (page images at HathiTrust)

• Tests of centrifugal pumps (New Mexico College of Agriculture and Mechanic Arts, 1911), by B. P. Fleming and J. B. Stoneking (page images at HathiTrust)
• Testing of pumps for use in nitric acid-alumina slurry service (U.S. Atomic Energy Commission, Idaho Operations Office, 1963), by E. J. Bailey, Idaho Chemical Processing Plant, Idaho National Reactor Testing Station, and Phillips Petroleum Company. Atomic Energy Division (page images at HathiTrust)
• Development of a mercury electromagnetic centrifugal pump for the SNAP-8 refractory boiler development program (National Aeronautics and Space Administration ;, 1974), by R. A. Fuller, A. W. Schnacke, Lewis Research Center, and General Electric Company (page images at HathiTrust)
• Design, manufacture, and test of coolant pump-motor assembly for Brayton power conversion system (National Aeronautics and Space Administration ;, 1973), by Louis E. Gebacz, Lewis Research Center, and Pesco Products Company (page images at HathiTrust)
• Centrifugal and rotary pumps (1903), by Albert Myron Johnson (page images at HathiTrust; US access only)
• Relation of speed of centrifugal pumps to height of lift (1906), by Edward J. Mehren (page images at HathiTrust; US access only)

• Three-step labyrinth seal for high-performance turbomachines (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987), by Robert C. Hendricks (page images at HathiTrust)
• Spin test of turbine rotor (National Aeronautics and Space Administration ;, 1972), by Michael H. Vavra, Lawrence E. Bell, James E. Hammer, United States National Aeronautics and Space Administration, and Naval Postgraduate School (U.S.) (page images at HathiTrust)
• NASA TN D-4393 (National Aeronautics and Space Administration ;, 1968), by Roy G. Stabe, John F. Kline, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental findings from zero-tank net positive suction head operation of the J-2 hydrogen pump (National Aeronautics and Space Administration ;, 1972), by Henry P. Stinson, Raymond J. Strickland, and George C. Marshall Space Flight Center (page images at HathiTrust)
• An experimental investigation of two-phase liquid oxygen pumping (National Aeronautics and Space Administration ;, 1973), by Loren A. Gross and George C. Marshall Space Flight Center. Astronautics Laboratory (page images at HathiTrust)
• Analytical and experimental study of dynamic characteristics of turbopumps (National Aeronautics and Space Administration ;, 1968), by H. Ohashi and George C. Marshall Space Flight Center (page images at HathiTrust)

• Centaur space vehicle pressurized propellant feed system tests. (National Aeronautics and Space Administration ;, 1972), by Lewis Research Center (page images at HathiTrust)
• Exploratory tests of two strut fuel injectors for supersonic combustion (National Aeronautics and Space Administration ;, 1974), by Griffin Y. Anderson, Paul B. Gooderum, and Langley Research Center (page images at HathiTrust)

• NASA TN D-4040 (National Aeronautics and Space Administration ;, 1967), by Charles E. Feiler, Marcus F. Heidmann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Noncavitating and cavitating performance of several low area ratio water jet pumps having throat lengths of 3.54 diameters (National Aeronautics and Space Administration ;, 1969), by Nelson L. Sanger, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Steam jet pump analysis and experiments (Washington, D.C. : Office of Technical Services, Department of Commerce, 1960., 1960), by Ronald P. Rose, Westinghouse Electric Corporation, U.S. Atomic Energy Commission, and Bettis Atomic Power Laboratory (page images at HathiTrust)
• Controlled tests of eductors and submersible pumps (U.S. Army Engineer Waterways Experiment Station, 1994), by James E. Clausner, Dredging Research Program, U.S. Army Engineer Waterways Experiment Station, and United States Army Corps of Engineers (page images at HathiTrust)

• Centrifugal and rotary pumps (1903), by Albert Myron Johnson (page images at HathiTrust; US access only)

• Controlled tests of eductors and submersible pumps (U.S. Army Engineer Waterways Experiment Station, 1994), by James E. Clausner, Dredging Research Program, U.S. Army Engineer Waterways Experiment Station, and United States Army Corps of Engineers (page images at HathiTrust)

• A technique for cryopumping hydrogen (National Aeronautics and Space Administration, 1961), by Jack Grobman and Lewis Research Center (page images at HathiTrust)

• Tests of the University pumps and wells (1906), by Norval Enger (page images at HathiTrust; US access only)

• Performance of a tandem-rotor/tandem-stator conical-flow compressor designed for a pressure ratio of 3 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Jerry R. Wood, Lawrence F. Schumann, Albert Kimsey Owen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Analytical and experimental study of flow phenomena in noncavitating rocket pump inducers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by B. Lakshminarayana, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)

• Effect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor (National Aeronautics and Space Administration ;, 1975), by Hugh A. Klassen and Lewis Research Center (page images at HathiTrust)
• Experimental performance of a 16.10-centimeter-tip-diameter sweptback centrifugal compressor designed for a 6:1 pressure ratio (National Aeronautics and Space Administration ;, 1977), by Hugh A. Klassen, Lawrence F. Schumann, Jerry R. Wood, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of a tandem-rotor/tandem-stator conical-flow compressor designed for a pressure ratio of 3 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Jerry R. Wood, Lawrence F. Schumann, Albert Kimsey Owen, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Performance of a low-pressure-ratio centrifugal compressor with four diffuser designs (National Aeronautics and Space Administration ;, 1973), by Hugh A. Klassen and Lewis Research Center (page images at HathiTrust)
• Design and tests of a six-stage axial-flow compressor having a tip speed of 550 feet per second and a flat operating characteristic at constant speed (National Advisory Committee for Aeronautics, 1958), by Willard R. Westphal, John W. Maynard, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Rotating stall investigation of the 0.72 hub-tip ratio single-stage compressor (National Advisory Committee for Aeronautics, 1954), by Robert W. Graham, Vasily D. Prian, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1944), by J. Austin King, Owen W. Regan, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

More items available under broader and related terms at left.