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Pressure transducers

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• Pressure -- Measurement
• Transducers

• Pressure sensors
• Transducers, Pressure

• Instrumentation, field operations, and data processing for PMEL deep ocean bottom pressure measurements / (Seattle, Wash. : U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Pacific Marine Environmental Laboratory ; Springfield, VA : For sale by the National Technical Information Service, [1989]), by M. C Eble and Pacific Marine Environmental Laboratory (U.S.) (page images at HathiTrust)
• Thin film oxygen partial pressure sensor / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by J. J. Wortman, Langley Research Center, and Research Triangle Institute (page images at HathiTrust)
• Wind-tunnel tests of seven static-pressure probes at transonic speeds / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Francis J. Capone, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Liquid-filled transient pressure measuring systems : a method for determining frequency respose / ([Washington, D.C.] : National Aeronautics and Space Administration, [Scientific and Technical Information Branch], [1971?]), by Robert C. Anderson, David R. Englund, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Transonic wind-tunnel tests of an error-compensated static-pressure probe / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Francis J. Capone, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Atmospheric pressure jumps measured with arrays of sensitive pressure sensors in the vicinity of Chicago's O'Hare International Airport / (Boulder, Colo. : U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, [1977]), by A. J. Bedard, Mary M. Cairns, Wave Propagation Laboratory, and Environmental Research Laboratories (U.S.) (page images at HathiTrust)
• Frequency response of two types of liquid-metal pressure transducers with standoff tubes / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Joseph S. Curreri, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Performance of two models of commercial unbonded strain-gage-type absolute pressure transducer at 260 ̊C / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1969), by Ralph D. Lewis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A small combination sensing probe for measurement of temperature, pressure, and flow direction / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by George E. Glawe, Thomas J. Dudzinski, Lloyd N. Krause, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Comparison of concurrent strain gage- and presure transducer-measured flight loads on a lifting reentry vehicle and correlation with wind tunnel predictions / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Ming Han Tang, Robert G. Sheldon, Walter J. Sefic, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Optical zero-differential pressure switch and its evaluation in a multiple-pressure measuring system / (Washington : National Aeronautics and Space Adinistration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by J. Anthony Powell and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Dynamic response of high-frequency pressure transducers to large amplitude sinusoidal pressure oscillations / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Richard E. Robinson, Lewis Research Center, and Battelle Memorial Institute (page images at HathiTrust)
• A feasibility study of a miniature solid-state pressure transducer / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by C. D. Parker, Research Triangle Institute, and Langley Research Center (page images at HathiTrust)
• High-temperature transient pressure transducer for use in liquid-metal systems / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Ted W. Nyland, Richard Ernest Chase, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• A miniature electromechanical tunnel diode transducer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Wilhelm Rindner, A. Iannini, E. Pittelli, A. Garfein, United States National Aeronautics and Space Administration, and Electronics Research Center (U.S.) (page images at HathiTrust)
• Acceleration compensated low level pressure transducer / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by Samuel Lederman and Marian Visich (page images at HathiTrust; US access only)
• Flight type oxygen partial pressure sensor / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by S. A. Sternbergh and W. M. Hickam (page images at HathiTrust; US access only)
• Feasibility of miniaturizing a heater for a thin-film oxygen partial-pressure sensor / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Carl R. Pearson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Methods for performance-testing of electromechanical pressure transducers / (Washington, D.C. : U.S. National Bureau of Standards : For sale by the Supt. of Docs., U.S. G.P.O., 1967), by Paul S. Lederer and United States. National Bureau of Standards (page images at HathiTrust)
• Summary report of pressure sensor for the loss of fluid test (LOFT) reactor / (Washington, D.C. : The Division, 1981), by T. R. Billeter, Hanford Engineering Development Laboratory, and Fuel Cycle U.S. Nuclear Regulatory Commission. Division of Safeguards (page images at HathiTrust)
• Final report Project Scooter : close-in pressure and shock arrival time measurements / (Livermore, Ca. : Lawrence Radiation Laboratory, 1961), by Jack N. Shearer, Otto H. Krause, Robert G. Olson, and Lawrence Radiation Laboratory (page images at HathiTrust)
• Experimental investigation of means for reducing the response of pressure transducers to thermal transients / (Washington : U.S. Dept. of Commerce, National Bureau of Standards : For sale by the Supt. of Docs., U.S. Govt. Print. Off., 1978), by John S. Hilten, Institute for Applied Technology (U.S.). Electronic Technology Division, United States. National Bureau of Standards. Technical note, and United States. Naval Air Systems Command (page images at HathiTrust)
• Transient behavior of lumped-constant systems for sensing gas pressures / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Gene J. Delio, Richard S. Cesaro, Glennon V. Schwent, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A theoretical examination of a variable reluctance diaphragm gage developed at Sandia Corporation / (Albuquerque, N.M. : Sandia Corporation, Technical Information Division ; Washington, D.C. : Available from the Office of Technical Services, Dept. of Commerce, [1960]), by George E. Reis and Sandia Corporation (page images at HathiTrust)
• Vibration effects on the Taylor 206R pressure transmitter,, by A. H. Fowler, G. H. Job, Carbide and Carbon Chemicals Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Vibration effects on the Taylor 206R pressure transmitter., by G. H. Job, J. A. Owen, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Flame-powered trigger device for activating explosion suppression barrier / (Washington, D.C. (2401 E St., N.W., Washington 20241-0001) : U.S. Dept. of the Interior, Bureau of Mines, 1991), by R. A. Cortese, M. J. Sapko, and United States Bureau of Mines (page images at HathiTrust)
• High temperature pressure transmitter evaluation / (Oak Ridge, Tenn. : Oak Ridge National Laboratory, 1958), by W. R. Miller, U.S. Atomic Energy Commission, Union Carbide Corporation, and Oak Ridge National Laboratory. Instrumentation and Controls Division (page images at HathiTrust)
• High temperature pressure transducer (Mk I) / (Los Alamos, N.M. : Los Alamos Scientific Laboratory of the University of California, 1962), by L. H. Thacker, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Sandia diaphragm-type pressure transducer for shock wave measurements / (Oak Ridge, Tenn. : Technical Information Extension ; Washington, D.C. : Available from the Office of Technical Services, Dept. of Commerce, [1954]), by Peter K. Church, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Multiple pressure transducer banks and their application /, by D. B. Risher and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Design and testing of a 100,000-psi eddy-current pressure transducer for hostile environments /, by John E. Field, U.S. Atomic Energy Commission, and Lawrence Radiation Laboratory (page images at HathiTrust)
• The design, development, and evaluation of a differential pressure gauge directional wave monitor /, by Kevin R. Bodge and Coastal Engineering Research Center (U.S.) (page images at HathiTrust)
• Pressure sensor for use in the Loss-of-Fluid-Test (LOFT) reactor /, by T. R. Billeter, United States. National Technical Information Service, Hanford Engineering Development Laboratory, and U.S. Nuclear Regulatory Commission (page images at HathiTrust)
• Summary report of fuel rod displacement sensor for LOFT /, by T. R Billeter, United States. National Technical Information Service, United States Government Printing Office, Hanford Engineering Development Laboratory, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
• The electronic pressure transmitter and self balancing relay / (Oak Ridge, Tenn. : Atomic Energy Commission, [1947]), by S. Cromer, U.S. Atomic Energy Commission, and Columbia University (page images at HathiTrust)

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

• Effects of Mach number on pitot-probe displacment in a turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Jerry M. Allen and Langley Research Center (page images at HathiTrust)
• Effects of geometric variables on the performance of a probe for direct measurement of free-stream stagnation pressure in supersonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Lana M. Couch and Langley Research Center (page images at HathiTrust)
• Pitot-probe displacement in a supersonic turbulent boundary layer (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1972), by Jerry M. Allen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Evaluation of compressible-flow Preston tube calibrations / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Jerry M. Allen and Langley Research Center (page images at HathiTrust)
• Pilot model expansion tunnel test flow properties obtained from velocity, pressure, and probe measurements (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Wilfred J. Friesen, John A. Moore, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calibration of pitot tubes / (1905), by Otto Kuehlcke (page images at HathiTrust; US access only)
• Calibration of pitot tubes / (1904), by John Frederick Peterson (page images at HathiTrust; US access only)
• Investigation of the effect of form of orifices for the Pitot tube / (1906), by Louis Solliday Knorr (page images at HathiTrust; US access only)
• Measurement of water surface roughness and wind shear stress by the use of a pitot tube in a laboratory wave channel / (Berkeley : University of California, Institute of Engineering Research, Waves Investigation Laboratory, 1954), by Osvald Sibul, Berkeley. Institute of Engineering Research. Waves Investigation Laboratory University of California, and United States Army Corps of Engineers (page images at HathiTrust)
• Pitot pressure measurements in flow fields behind circular-arc nozzles with exhaust jets at subsonic free-stream mach numbers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : for sale by the National Technical Information Service], 1979), by Mary L. Mason, Lawrence E. Putnam, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Reevaluation of compressible-flow Preston tube calibrations / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Jerry M. Allen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A flight evaluation of a trailing anemometer for low-speed calibrations of airspeed systems on research aircraft / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Bruce D. Fisher, H. Paul Stough, Bruce J. Holmes, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Measurement of upper-atmosphere structure by means of the pitot-static tube / (Washington : National Aeronautics and Space Administration, [1961]), by J. E. Ainsworth, H. E. LaGow, D. F. Fox, and Goddard Space Flight Center (page images at HathiTrust)
• Experimental laminar, transitional, and turbulent boundary-layer profiles on a wedge at local Mach number 6.5 and comparisons with theory / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Michael C. Fischer, Dal V. Maddalon, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental preston tube and law-of-the-wall study of turbulent skin friction on axisymmetric bodies at supersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Jerry M. Allen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Accuracy of pitot-pressure rakes for turbulent boundary-layer measurements in supersonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by Earl R. Keener, Edward J. Hopkins, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by use of accelerometer and attitude-angle measurements / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by John A. Zalovcik and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Separated flow phenomena on a slender cone at Mach 5 /, by Robert H. Feldhuhn, Allen E. Winkelmann, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• An experimental investigation of the laminar boundary layer on a spinning ogive cylinder in supersonic flow /, by William C. Ragsdale, Robert G. Ball, Michael A. Brown, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Wind-tunnel calibration of a combined pitot-static tube and vane-type flow-angularity indicator at Mach numbers of 1.61 and 2.01 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by Archibald R. Sinclair, William D. Mace, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Accuracy of airspeed measurements and flight calibration procedures / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by Wilber B. Huston and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparison of airspeed calibrations evaluated by the accelerometer and radar methods / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Lindsay J. Lina, James P. Trant, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An experimental investigation of the surface Pitot probe including effects of heat transfer and compressibility /, by David L. Brott, Roland E. Lee, William Joseph Yanta, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)

More items available under broader and related terms at left.