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Superchargers -- Testing

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• Superchargers
• Compressors -- Testing
• Internal combustion engines -- Testing
• Testing

• 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)

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

• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by William A. Benser, Jason J. Moses, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Supercharging the internal combustion engine. (McGraw-Hill Book Co., 1948), by Edward Thomas Vincent (page images at HathiTrust)

• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by William K. Ritter, Irving A. Johnsen, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (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)

• Superchargers for aviation (National aeronautics council, Inc., 1942), by Sanford A. Moss and National Aeronautics Council (U.S.) (page images at HathiTrust)
• Allison service school handbook, Allison V-1710 engines models "E" and "F" (Indianapolis, Indiana, U.S.A. : Allison Division, General Motors Corporation, 1943., 1943), by General Motors Corporation. Allison Division (page images at HathiTrust)
• Calculations of the performance of a compression-ignition engine-compressor turbine combination. [Part] 2, Performance of complete combination (National Advisory Committee for Aeronautics, 1947), by Alexander Mendelson, United States National Advisory Committee for Aeronautics, and Aircraft Engine Research Laboratory (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by William K. Ritter, Irving A. Johnsen, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by J. Austin King, Harold Klein, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), by Aircraft Engine Research Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1945), by J. C. Sanders, Alexander Mendelson, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), by Earl E. Coulter, David S. Gabriel, Robert G. Larkin, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1946), by Edmund J. Baas, Paul D. Dugan, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series L. (National Advisory Committee for Aeronautics, 1942), by George P. Wood, D. E. Brimley, Langley Aeronautical Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)

• Field and depot maintenance for engine, diesel (multifuel), turbosupercharged, fuel injected, water cooled, 6-cylinder, assembly-2815-897-5061, (Continental model LDS-427-2) and clutch, assembly (ORD 7748995), (Long model 13CF) : end item application, truck, cargo, 2 1/2 ton, 6 x 6, M35A1, (multifuel)--(TM 9-2320-235). (Headquarters, Dept. of the Army, 1989), by United States. Department of the Army (page images at HathiTrust)
• Direct support, general support and depot maintenance manual, including repair parts and special tools lists for engine, with container, turbosupercharged, diesel, fuel injection, 90-degree "V" type, air cooled, 12-cylinder, assembly; models AVDS-1790-2M (2815-856-4996), AVDS-1790-2A and AVDS-1790-2AM (2815-856-9005). (Headquarters, Dept. of the Army, 1989), by United States. Department of the Army (page images at HathiTrust)
• Direct support and general support maintenance manual for engine, with container, turbosupercharged, diesel, fuel injection, 90-degree "V" type, air-cooled, 12-cylinder, assembly; models AVDS-1790-2C, 2815-00-410-1203 and AVDS-1790-2D, 2815-00-410-1204. (Headquarters, Dept. of the Army, 1990), by United States. Department of the Army (page images at HathiTrust)
• Direct support and general support maintenance repair parts and special tools lists (including depot maintenance repair parts and special tools) : engine, with container, turbosupercharged, diesel, fuel injection, 90-degree "V" type, air-cooled, 12-cylinder, assembly; models AVDS-1790-2C, 2815-00-410-1203 and AVDS-1790-2D, 2815-00-410-1204 and AVDS-1790-2DR, 2815-00-124-5387. (Headquarters, Dept. of the Army, 1992), by United States. Department of the Army (page images at HathiTrust)

• The development and introduction of the automotive turbocharger : a case of innovation in response to fuel economy regulation (The Office ;, 1979), by Larry Ronan, William J. Abernathy, Transportation Systems Center, Lexington Technology Associates, and United States. National Highway Traffic Safety Administration. Research and Development (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)

• 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)

• 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)

• 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)

• Automotive engine testing; a manual of test procedure (Pitman Pub. Corp., 1940), by Foster M. Gruber (page images at HathiTrust)
• The testing of high speed internal combustion engines : with special reference to automobile and aircraft types, and to the testing of automobiles (Van Nostrand, 1925), by Arthur William Judge (page images at HathiTrust)
• The testing of internal combustion engines, by S.J. Young ... and R. W. J. Pryer ... (D.Van Nostrand company, inc., 1937), by Sydney John Young and Robert William John Pryer (page images at HathiTrust)
• The testing of high speed internal combustion engines, with special reference to automobile and aircraft types and to the testing of automobiles (D. Van Nostrand company, inc., 1932), by Arthur William Judge (page images at HathiTrust)
• Testing of the LaForce engine by the Environmental Protection Agency staff report prepared for the Committee on Commerce, U.S. Senate (U.S. Govt. Print. Off., 1975), by Barry I. Hyman and United States Senate Committee on Commerce (page images at HathiTrust)
• The testing of high speed internal combustion engines, with special reference to automobile and aircraft types, and to the testing of automobiles (Chapman & Hall, 1924), by Arthur William Judge (page images at HathiTrust; US access only)
• Die Gasmaschine : insonderheit die Viertakt-Gasmaschine, ihre Untersuchung auf Wirtschaftlichkeit und Leistung und Beschreibung der dazu nötigen Instrumente (F. Vieweg und Sohn, 1908), by Arthur Eckardt (page images at HathiTrust)
• Tests of a Bogart gas engine (1913), by Martin Ira Mix, Roscoe Conkling Harris, and Paul Hedges Gibbs (page images at HathiTrust; US access only)
• A thermodynamic analysis of gas engine tests (University of Illinois, 1925), by Crandall Zachariah Rosecrans and George Theodore Felbeck (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), by Arnold E. Biermann, Lester C. Corrington, Aircraft Engine Research Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• NACA Wartime Reports. Series E. (National Advisory Committee for Aeronautics, 1943), by Aircraft Engine Research Laboratory and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Internal-combustion engines: power test codes. (New York, 1957), by American Society of Mechanical Engineers (page images at HathiTrust; US access only)
• Calibration procedure for internal combustion engine tester (general). (Headquarters, Dept. of the Army, 1984), by United States. Department of the Army (page images at HathiTrust)

More items available under broader and related terms at left.