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Compressors -- Valves -- Testing

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• Compressors -- Valves
• Compressors -- Testing
• Valves -- Testing

• Calibration procedure for compressor bleed valve test stand, Lycoming, model LTCT421. (Headquarters, Dept. of the Army, 1984), by United States. Department of the Army (page images at HathiTrust)

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

• 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)

• A computer program for variable-geometry single-stage axial compressor test data analysis (UD0400) (Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1981), by C. Herbert Law and Air Force Wright Aeronautical Laboratories. Aero Propulsion Laboratory (page images at HathiTrust)

• Optimization of compressor vane and bleed settings (Aero Propulsion Laboratory, Wright Aeronautical Laboratories, Air Force Systems Command, 1981), by J. E. Garberoglio, W. L. Bourdreaux, J. O. Song, and Pratt & Whitney Aircraft Group. Government Products Division (page images at HathiTrust)

• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by Aircraft Engine Research Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• A comparison of sound power levels from portable air compressors based upon test methodologies adopted by U.S. EPA and the CEC. (U.S. Environmental Protection Agency, Office of Noise Abatement and Control ;, 1980), by Commission of the European Communities. Environment and Consumer Protection Service and United States Office of Noise Abatement and Control (page images at HathiTrust)

• Inspection and test of air and other gas compressors. (Headquarters, Dept. of the Army, 1991), by United States. Department of the Army (page images at HathiTrust)

• Design and performance of a high-pressure-ratio, highly loaded axial-flow transonic compressor space (National Aeronautics and Space Administration ;, 1974), by George W. Lewis, Edward R. Tysl, Lonnie Reid, and Lewis Research Center (page images at HathiTrust)
• Frequency response of an axial-flow compressor exposed to inlet pressure perturbations (National Aeronautics and Space Administration ;, 1974), by Edward J. Milner, Francis J. Paulovich, Leon M. Wenzel, and Lewis Research Center (page images at HathiTrust)
• Performance of a transonic compressor rotor with an aspect ratio of 6.5 (National Aeronautics and Space Administration ;, 1974), by Lonnie Reid, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)

• Performance of a 1.15-pressure-ratio axial-flow fan stage with a blade tip solidity of 0.5 (National Aeronautics and Space Administration ;, 1974), by Walter Martin Osborn, Ronald J. Steinke, and Lewis Research Center (page images at HathiTrust)

• 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)

• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1942), by Herman H. Ellerbrock, Arthur W. Goldstein, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine (National Advisory Committee for Aeronautics, 1955), by Reeves P. Cochran, Robert P. Dengler, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, 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)

• 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)

• Inspection and test of air and other gas compressors. (Headquarters, Dept. of the Army, 1991), by United States. Department of the Army (page images at HathiTrust)

• Final report on the development and testing of the robovalve (Dept. of State], Agency for International Development, 1978), by Yaron M. Sternberg, Robert Knight, University of Maryland. International Rural Water Resources Development Laboratory, and United States. Agency for International Development (page images at HathiTrust)
• Response of a 4-inch nuclear power plant valve to dynamic excitation (The Commission :, 1980), by S. F. Masri, S. J. Stott, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• Erosion testing of potential valve materials for coal gasification systems (Dept. of the Interior, Bureau of Mines, 1979), by J. S. Hansen, F. W. Wood, and John E. Kelley (page images at HathiTrust)
• Filling and emptying system, Walter Bouldin Lock, and lock culvert valve for Coosa River Waterway, Alabama : hydraulic model investigation (Dept. of the Army, Waterways Experiment Station, Corps of Engineers ;, 1984), by John F. George and U.S. Army Engineer Waterways Experiment Station (page images at HathiTrust)
• 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)
• Reclamation of defective hoke diaphragm type packless valves (Oak Ridge, TN : K-25 Plant, Carbide and Carbon Chemicals Corporation, 1949., 1949), by N. H. Pease, U.S. Atomic Energy Commission, and Carbide and Carbon Chemicals Corporation (page images at HathiTrust)
• Fixed-cone valve prototype tests, final series, New Melones Dam, California (Vicksburg, Mississippi : U.S. Army Engineer Waterways Experiment Station ; [Springfield, Virginia] : [Available from National Technical Information Service], 1984., 1984), by Timothy L. Fagerburg, Waterways Experiment Station (U.S.), and U.S. Army Engineer Waterways Experiment Station (page images at HathiTrust)
• Tests on 24-inch hollow-jet valve at Boulder Dam (U.S. Dept. of the Interior, Bureau of Reclamation, 1945), by Fred Locher and United States Bureau of Reclamation (page images at HathiTrust)
• Hydraulic tests and development of multijet sleeve valves (Hydraulics Branch, Division of General Research, Engineering and Research Center, U.S. Dept. of the Interior, Bureau of Reclamation ;, 1977), by P. H. Burgi and Engineering and Research Center. Hydraulics Branch (page images at HathiTrust)
• Retest and evaluation of antiblast valves (Washington, D.C. : Civil Effects Test Operations, 1959., 1959), by James E. Roembke and U.S. Atomic Energy Commission. Civil Effects Test Operations Office (page images at HathiTrust)

• Leakage of water from valve stuffing boxes (E.I. du Pont de Nemours & Co., Explosives Dept., Atomic Energy Division, Technical Division, Savannah River Laboratory, 1961), by Frederick C. Apple, U.S. Atomic Energy Commission, Savannah River Laboratory, and E.I. du Pont de Nemours & Company (page images at HathiTrust)
• Thermal cycling and leakage tests of 2 inch valves for sodium service (Atomics International, 1960), by C. J. Baroczy, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• The selection, design modification, and analysis of sodium valves for Hallam Nuclear Power Facility (Atomics International, 1960), by B. Brooks, F. Bergonzoli, R. Galantine, North American Aviation. Atomics International Division, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Equipment qualification research : test program and failure analysis of class 1E solenoid valves (Washington, D. C. : Division of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1983., 1983), by D. V. Paulson, S. P. Carfagno, V. P. Bacanskas, T. A. Shook, Franklin Research Center, and U.S. Nuclear Regulatory Commission. Office of Inspection and Enforcement. Division of Emergency Preparedness and Engineering Response (page images at HathiTrust)

• Test of 6" model outlet regulating valve : for Yuba Manufacturing Division, Yuba Consolidated Industries, Inc. (University of California, Institute of Engineering Research, 1959), by H. W. Iversen and Berkeley. Institute of Engineering Research University of California (page images at HathiTrust; US access only)