Books on the topic 'Cryogenic measurement'

A, Richard M., Antenna Measurement Techniques Association. Meeting and Symposium., National Institute of Standards and Technology (U.S.), and United States. National Aeronautics and Space Administration., eds. Measurement techniques for cryogenic Ka-band microstrip antennas. [Washington, D.C: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Effect of vaporization on cryogenic spray dropsize measurement. [Washington, DC: National Aeronautics and Space Administration, 1992.

United States. National Aeronautics and Space Administration., ed. On the relationship between Schottky barrier capacitance and mixer performance at cryogenic temperatures. [Washington, DC: National Aeronautics and Space Administration, 1996.

V, Delcourt, Plazanet M, and United States. National Aeronautics and Space Administration., eds. Problems associated with operations and measurement in cryogenic wind tunnels. Washington DC: National Aeronautics and Space Administration, 1986.

V, Delcourt, Plazanet M, and United States. National Aeronautics and Space Administration., eds. Problems associated with operations and measurement in cryogenic wind tunnels. Washington DC: National Aeronautics and Space Administration, 1986.

Chapman, John J. A hybrid electronically scanned pressure module for cryogenic environments. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Chapman, John J. A hybrid electronically scanned pressure module for cryogenic environments. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

H, Fabik Richard, and United States. National Aeronautics and Space Administration., eds. Techniques for improving the accuracy of cryogenic temperature measurement in ground test programs. [Washington, DC: National Aeronautics and Space Administration, 1993.

C, Rogers A., and United States. National Aeronautics and Space Administration., eds. Compression mass gauge testing in a liquid hydrogen dewar. [Washington, D.C.?]: National Aeronautics and Space Administration, 1995.

Dechene, Ronald L. Mass flow measurement of liquid cryogens using the triboelectric effect: NASA contract NA83-24873, final report, August 12, 1986. Danvers, Mass: Auburn International, Inc., 1986.

McElroy, Frank F. A cryogenic preconcentration: Direct FID (PDFID) method for measurement of NMOC in ambient air. Research Triangle Park, N.C: U.S. Environmental Protection Agency, Environmental Monitoring Systems Laboratory, 1986.

M, Jurns John, Chato David J, and United States. National Aeronautics and Space Administration., eds. LN spray droplet size measurement via ensemble diffraction technique. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

W, Edwards John, and Langley Research Center, eds. Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Johnson, Charles B. Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-meter transomic cryogenic tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Johnson, Charles B. Dynamic measurement of total temperature, pressure, and velocity in the Langley 0.3-Meter Transonic Cryogenic Tunnel. Hampton, Va: Langley Research Center, 1986.

Murthy, A. V. Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter Transonic Cryogenic Tunnel. Hampton, Va: Langley Research Center, 1988.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Bernatowicz, H. Mass flow meter using the triboelectric effect for measurement in cryogenics: NASA contract NAS324648 : final report, April, 1987. Sunnyvale, CA: Science Applications International Corporation, 1987.

United States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. San Jose, CA: MCAT Institute, 1991.

United States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. San Jose, CA: MCAT Institute, 1992.

United States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle. San Jose, CA: MCAT Institute, 1993.

United States. National Aeronautics and Space Administration., ed. Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle: Final report. San Jose, CA: MCAT Institute, 1995.

T, Weber Theodore, and Ames Research Center, eds. Cryogenic measurements of aerojet GaAs n-JFETs. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

R, Buchele Donald, and United States. National Aeronautics and Space Administration., eds. Scattered-light scanner measurements of cryogenic liquid-jet breakup. [Washington, D.C: National Aeronautics and Space Administration, 1990.

R, Buchele Donald, and United States. National Aeronautics and Space Administration., eds. Scattered-light scanner measurements of cryogenic liquid-jet breakup. [Washington, D.C: National Aeronautics and Space Administration, 1990.

Ingebo, Robert D. Scattered-light scanner measurements of cryogenic liquid-jet breakup. [Washington, D.C: National Aeronautics and Space Administration, 1990.

P, Boyden Richmond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Aerodynamic measurements and thermal tests of a strain-gage balance in a cryogenic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

DeLombard, Richard. SAMS acceleration measurements on Mir from January to May 1997 (NASA Increment 4). [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Center, Lewis Research, ed. SAMS acceleration measurements on Mir from January to May 1997 (NASA Increment 4). [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

United States. National Aeronautics and Space Administration., ed. Influence of temperature and impact velocity on the coefficient of restitution. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Influence of temperature and impact velocity on the coefficient of restitution. [Washington, DC]: National Aeronautics and Space Administration, 1994.

L, Lawing Pierce, and Langley Research Center, eds. Measurements in the flow field of a cylinder with a laser transit anemometer and a drag rake in the Langley 0.3 m Transonic Cryogenic Tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Richard C. Smelser Peter Muhlenhaupt. Carbon Resistors for Cryogenic Liquid Level Measurement; NBS Technical Note 200. Creative Media Partners, LLC, 2021.

Temperature and pressure effects on capacitance probe cryogenic liquid level measurement accuracy. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Sidewall boundary-layer measurements with upstream suction in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Cohadon, Pierre-François, Jack Harris, Florian Marquardt, and Leticia Cugliandolo, eds. Quantum Optomechanics and Nanomechanics. Oxford University Press, 2020. http://dx.doi.org/10.1093/oso/9780198828143.001.0001.

Cryogenic measurements of aerojet GaAs n-JFETs. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1993.

Scattered-light scanner measurements of cryogenic liquid-jet breakup. [Washington, D.C: National Aeronautics and Space Administration, 1990.

Cryogenic probe station for use in automated microwave and noise figure measurements. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Analysis of fluctuating static pressure measurements in a large high Reynolds number transonic cryogenic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, 1993.

National Aeronautics and Space Administration (NASA) Staff. Sidewall Boundary-Layer Measurements with Upstream Suction in the Langley 0. 3-Meter Transonic Cryogenic Tunnel. Independently Published, 2018.

Calculation of sidewall boundary-layer parameters from rake measurements for the Langley 0.3-meter transonic cryogenic tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.