Compressors -- Testing -- ProcedureSee also what's at your library, or elsewhere.
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Filed under: Compressors -- Testing -- Procedure
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Filed under: Compressors -- Testing- 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)
Filed under: Compressors -- Testing -- Computer programsFiled under: Compressors -- Testing -- Data processingFiled under: Air-compressors -- Testing
Filed under: Air-compressors -- Testing -- Handbooks, manuals, etc.Filed under: Axial flow compressors -- Testing- 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)
Filed under: Axial flow compressors -- Testing -- StatisticsFiled 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: Superchargers -- TestingFiled under: Airplanes -- Turbojet engines -- Compressors -- Testing- 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)
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: Compressors -- United States -- Testing -- Handbooks, manuals, etc.Filed under: Compressors -- Valves -- Testing
Filed under: Procedure
Filed under: Procedure -- Austria
Filed under: Procedure -- Bengal
Filed under: Procedure -- Bolivia
Filed under: Procedure -- Brazil
Filed under: Procedure -- Civil
Filed under: Procedure -- Criminal
Filed under: Procedure -- Egypt
Filed under: Procedure -- France
Filed under: Procedure -- General
Filed under: Procedure -- Germany- Die gesammten Materialien zu den Reichsjustizgesetzen. Auf Veranlassung des Kaiserlichen Reichs-justizamts (R.v. Decker, 1879), by Carl Hahn, E. Stegemann, B. Mugdan, Germany. Reichstag, and Germany. Reichsjustizamt (page images at HathiTrust)
- Die Angelegenheiten der freiwilligen Gerichtsbarkeit: Reichsgesetz vom 17./20. Mai 1898, preussisches Gesetz vom 21. September 1899 ... (C. Heymann, 1900), by Germany, Rudolf Schultze-Görlitz, and Hermann Oberneck (page images at HathiTrust)
- Bürgerliche gesetzbuch (C. Heymann, 1901), by Pierre Siméon (page images at HathiTrust)
- Das verwaltungsstreitverfahren. Praktisches handbuch auf wissenschaftlicher grundlage (J. Guttentag, g.m.b.h., 1908), by Fritz Kunze (page images at HathiTrust)
- Zur Lehre von der materiellen Rechtskraft in Verwaltungssachen (A. Edelmann, 1906), by Otto Mayer (page images at HathiTrust)
- Informativprozesse. Anregungen zu einer ergänzung der prozessgesetzgebung (Alfred Töpelmann, 1907), by Ernst Beling (page images at HathiTrust)
- Unser gerichtswesen. (Stuttgart, 1906), by Alexander von Harder (page images at HathiTrust)
- Zur lehre von dem mangel der prozessfähigkeit, der legitimation als gesetzlicher vertreter und der prozessvollmacht nach deutschem civilprozessrechte ([Berlin, 1906), by Friedrich Hellmann (page images at HathiTrust)
- Der gegenstand der rechtskraft (F. Meiner, 1913), by Georg Kleinfeller (page images at HathiTrust; US access only)
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