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Ejector pumps -- Design and construction

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• Ejector pumps
• Design and construction

• Improved eductors for sand bypassing (U.S. Army Engineer Waterways Experiment Station, 1994), by Gregory L. Williams, Peter Jay Neilans, James E. Clausner, Dredging Research Program, U.S. Army Engineer Waterways Experiment Station, and United States Army Corps of Engineers (page images at HathiTrust)

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

• The efficiency of pumps and ejectors (Van Nostrand, 1920), by Edward Cyril Bowden-Smith (page images at HathiTrust)
• Venturi air-jet vacuum ejectors for high-volume atmospheric sampling on aircraft platforms (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Gerald Franklin Hill and Langley Research Center (page images at HathiTrust)
• NASA TN D-5810 (National Aeronautics and Space Administration :, 1970), by Lawrence F. Hatakeyama, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6160 (National Aeronautics and Space Administration :, 1971), by Francis C. Chenoweth (page images at HathiTrust; US access only)
• Performance investigation of a nonpumping rocket-ejector system for altitude simulation (National Aeronautics and Space Administration, 1959), by Anthony Fortini and Lewis Research Center (page images at HathiTrust)
• Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles (National Aeronautics and Space Administration, 1960), by Laurence W. Gertsma, Richard A. Yeager, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of free-stream Mach number on gross-force and pumping characteristics of several ejectors (National Advisory Committee for Aeronautics, 1955), by Leonard E. Stitt, Alfred S. Valerino, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles (National Advisory Committee for Aeronautics, 1956), by Donald P. Hearth, Robert W. Cubbison, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• An investigation of the water pressure ejector (1908), by Mark Ross Haynes (page images at HathiTrust; US access only)
• Characteristics of five ejector configurations at free-stream mach numbers from 0 to 2.0 (National Aeronautics and Space Administration, 1959), by John L. Klann, Ronald G. Huff, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transonic off-design performance of a fixed divergent ejector designed for a mach number of 2.0 (National Aeronautics and Space Administration, 1959), by Harry T. Norton, Charles E. Mercer, Marlowe D. Cassetti, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Eductors in hydraulic systems. ([University Park, Pa.], 1955), by Albrecht W. Hussmann (page images at HathiTrust; US access only)
• The Alperin jet-diffuser ejector (AJDE) development, testing, and performance verification report (China Lake, California : Naval Weapons Center, Systems Development Department, 1976., 1976), by Morton Alperin, Charles A. Smith, Kiunn Jenq Wu, United States. Naval Air Systems Command, and Naval Weapons Center (page images at HathiTrust)
• Steady flow ejector research program; final report for extended contract Nonr-3067(00) [by] J.K. Johnson, Jr., P.K. Shumpert [and] J.F. Sutton. ([Marietta, Ga.?], 1961), by Lockheed-Georgia Company, J. F. Sutton, P. K. Shumpert, and J. K. Johnson (page images at HathiTrust; US access only)

• Performance and noise generation studies of supersonic air ejectors (National Aeronautics and Space Administration ;, 1972), by P. S. Barna, Langley Research Center, and Old Dominion University (page images at HathiTrust)

• Performance and noise generation studies of supersonic air ejectors (National Aeronautics and Space Administration ;, 1972), by P. S. Barna, Langley Research Center, and Old Dominion University (page images at HathiTrust)

• Analysis and testing of two-dimensional vented Coanda ejectors with asymmetric variable area mixing sections (National Aeronautics and Space Administration ;, 1976), by Dynatech Corporation, Lewis A. Maroti, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Performance and noise generation studies of supersonic air ejectors (National Aeronautics and Space Administration ;, 1972), by P. S. Barna, Langley Research Center, and Old Dominion University (page images at HathiTrust)
• Analysis and testing of two-dimensional slot nozzle ejectors with variable area mixing sections (National Aeronautics and Space Administration ;, 1973), by Gerald B. Gilbert, Philip G. Hill, Ames Research Center, and Dynatech R/D Company (page images at HathiTrust)
• Experimental study of zero-flow ejectors using gaseous nitrogen (National Aeronautics and Space Administration, 1960), by William Leroy Hill Jones, Carl F. Lorenzo, Harold G. Price, and Lewis Research Center (page images at HathiTrust)
• Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 (National Aeronautics and Space Administration, 1961), by Andrew J. Stofan, James R. Mihaloew, Lewis Research Center, and United States National Aeronautics and Space Administration (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)

• Hydraulic model investigation (Waterways Experiment Station ;, 1991), by Winston Glenn Davis, Robert A. Davidson, U.S. Army Engineer Waterways Experiment Station, and United States. Army. Corps of Engineers. St. Louis District (page images at HathiTrust)

• A design for a university library (1910), by Robert Guy Van Doren (page images at HathiTrust; US access only)

• An impulse accelerometer (Lawrence Radiation Laboratory, 1964), by William E. Nelson, G. Wayne Brown, and Lawrence Radiation Laboratory (page images at HathiTrust)
• The design and construction of a recording accelerometer (1909), by Robert Beam Rodgers (page images at HathiTrust; US access only)

• A fast-acting electrical servo for the actuation of full-span, Fowler-type wing flaps in DLC applications : a detail design study / by Frederick O. Smetana, Rafael J. Montoya, and Ronald K. Carden. (National Aeronautics and Space Administration ;, 1972), by Frederick O. Smetana, Ronald K. Carden, Rafael J. Montoya, Langley Research Center, and North Carolina State University (page images at HathiTrust)

• Digital adaptive flight controller development (National Aeronautics and Space Administration ;, 1974), by Howard Kaufman, Langley Research Center, and Rensselaer Polytechnic Institute. Systems Engineering Division (page images at HathiTrust)
• F-8C adaptive flight control extensions (National Aeronautics and Space Administration ;, 1977), by Günter Stein, Gary L. Hartmann, Honeywell Inc, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On the design of a high-gain saturating control system for use as an adaptive autopilot (National Aeronautics and Space Administration, 1960), by John D. McLean, Stanley F. Schmidt, and Ames Research Center (page images at HathiTrust)

• Design and development of the spinning mode synthesizer (National Aeronautics and Space Administration ;, 1973), by John M. Seiner, Gerhard Reethof, Langley Research Center, and Pennsylvania State University (page images at HathiTrust)

• A smoke generator system for aerodynamic flight research (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), by David M. Richwine, Gene V. Tracy, Robert E. Curry, and Dryden Flight Research Facility (page images at HathiTrust)

• An assessment of airfoil design by numerical optimization (National Aeronautics and Space Administration ;, 1974), by R. M. Hicks, Garret N. Vanderplaats, Earll M. Murman, and Ames Research Center (page images at HathiTrust)
• Application of numerical optimization to the design of low-speed airfoils (National Aeronautics and Space Administration ;, 1975), by R. M. Hicks, Garret N. Vanderplaats, and Ames Research Center (page images at HathiTrust)
• Transonic airfoil design using cartesian coordinates (U.S. National Aeronautics and Space Administration ;, 1976), by Leland A. Carlson, Texas A. and M. Research Foundation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A modified Theodorsen [epsilon]-function airfoil design procedure (National Aeronautics and Space Administration ;, 1974), by Raymond L. Barger and Langley Research Center (page images at HathiTrust)
• Low-speed aerodynamic characteristics of an airfoil optimized for maximum lift coefficient (National Aeronautics and Space Administration ;, 1972), by Gene J. Bingham, Allen Wen-shin Chen, and Langley Research Center (page images at HathiTrust)
• Effect of variable thermal properties on one-dimensional heat transfer in radiating fins (National Aeronautics and Space Administration, 1963), by Norbert O. Stockman, John L. Kramer, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On the use of thick-airfoil theory to design airfoil families in which thickness and lift are varied independently (National Aeronautics and Space Administration ;, 1974), by Raymond L. Barger and Langley Research Center (page images at HathiTrust)
• A streamline curvature method for design of supercritical and subcritical airfoils (National Aeronautics and Space Administration ;, 1974), by Raymond L. Barger, Cuyler W. Brooks, and Langley Research Center (page images at HathiTrust)
• Analytic airfoil analysis : design program (Wright Patterson Air Force Base, Ohio : Flight Dynamics Directorate , Wright Laboratory, Air Force Materiel Command, United States Air Force, 1994., 1994), by D. Stookesberry, W. Romer, J. Johnson, Y. Ikeda, A. Cain, A. Verhoff, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and McDonnell Douglas Astronautics Company-St. Louis (page images at HathiTrust)

• Human factors for flight deck certification personnel (U.S. Department of Transportation, Federal Aviation Administration, Research and Development Service ;, 1993), by M. Stephen Huntley, Kim M. Cardosi, and United States. Federal Aviation Administration. Research and Development Service (page images at HathiTrust)
• Radium hazard in a military aircraft instrument shop : final report (San Francisco, California : U.S. Naval Radiological Defense Laboratory, 1951., 1951), by R. K. Skow, Willa Wadleigh, O. J. Sobol, U.S. Naval Radiological Defense Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Training evaluation of an instrument panel homogeneous with respect to the principle of the moving part (Wright-Patterson Air Force Base, Ohio, Aero Medical Laboratory, Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1957., 1957), by Robert C. Houston, M. R. Green, United States. Air Force. Air Research and Development Command, Wright Air Development Center, Aerospace Medical Laboratory (U.S.), and University of Illinois (Urbana-Champaign campus). Aviation Psychology Laboratory (page images at HathiTrust)
• Psychological variables in the design of flight simulators for training (Wright-Patterson Air Force Base, Ohio, Aero Medical Laboratory, Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1959., 1959), by F. A. Muckler, United States. Air Force. Air Research and Development Command, Wright Air Development Center, Aerospace Medical Laboratory (U.S.), and University of Illinois (Urbana-Champaign campus). Aviation Psychology Laboratory (page images at HathiTrust)
• Instrumentation package for inflight physiological studies (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by M. N. Goldberg, W. V. Blockley, R. A. Mills, Aerospace Medical Laboratory, North American Aviation, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Influence of friction in making settings on a linear scale (Wright-Patterson Air Force Base, Ohio : United States, Air Force, Air Materiel Command, 1949., 1949), by William Leroy Jenkins, David Rigler, Louis O. Maas, Lehigh University, and United States. Air Force. Air Matériel Command (page images at HathiTrust)

• Full committee hearing on H.R. 5627, H.R. 7328, H.R. 7541, H.R. 1433, S.J. Res. 34, H.R. 2326, and H.R. 5632 ([U.S. G.P.O.], 1954), by United States House Committee on Armed Services (page images at HathiTrust)
• Subcommittee hearing on H.R. 7328, to promote the national defense by authorizing the construction of aeronautical research facilities by the National Advisory Committee for Aeronautics necessary to the effective prosecution of aeronautical research, H.R. 5627, to amend Public Law 472, 81st Congress, approved April 11, 1950, entitled "An act to promote the national defense and to contribute to more effective aeronautical research by authorizing professional personnel of the National Advisory Committee for Aeronautics to attend accredited graduate schools for research and study", and H.R. 7541, to promote the national defense by including a representative of the Department of Defense as a member of the National Advisory Committee for Aeronautics ([U.S. G.P.O.], 1954), by United States. Congress. House. Committee on Armed Services. Subcommittee No. 1 (page images at HathiTrust)
• Full committee hearing on H.R. 662, H.R. 1199, H.R. 1200, H.R. 1201, H.R. 1203, H.R. 2736, H.R. 2737, H.R. 1179, H.R. 2735, H.R. 1181, H.R. 1215, H.R. 1216, S. 927, H.R. 3911 ([U.S. G.P.O.], 1951), by United States House Committee on Armed Services (page images at HathiTrust)

More items available under broader and related terms at left.