Pressure measurementSee also what's at your library, or elsewhere.
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Filed under: Pressure measurement Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1976), by Marjorie E. Manro, Langley Research Center, and Boeing Commercial Airplane Company (page images at HathiTrust) Analysis and testing of high entrainment single nozzle jet pumps with variable mixing tubes / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Kenneth E. Hickman, Gerald B. Gilbert, Philip G. Hill, Langley Research Center, and Dynatech R/D Company (page images at HathiTrust) Laminar heat-transfer and pressure measurements at a Mach number of 6 on a sharp and blunt 15° half-angle cones at angles of attack up to 90° / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Raul J. Conti, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust) Aerodynamic performance of a fully film cooled core turbine vane tested with cold air in a two-dimensional cascade / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by Roy G. Stabe, John F. Kline, and Lewis Research Center (page images at HathiTrust) Flight measurement of wall-pressure fluctuations and boundary-layer turbulence / (Washington [D.C.] : National Aeronautics and Space Administration, 1960), by Harold R. Mull, Joseph S. Algranti, and Lewis Research Center (page images at HathiTrust) Correction of pressure data for thermal transpiration effects in pneumatic lines / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by James A. Daggerhart, Langley Research Center, and North Carolina State University (page images at HathiTrust) An approximate method for calculating surface pressures on curved profile blunt plates in hypersonic flow / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Marcus O. Creager and Ames Research Center (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)
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