Books on the topic 'Test temperature'

Knoll, Richard H. Design, development, and test of shuttle/Centaur G-prime cryogenic tankage thermal protection systems. [Washington, DC: National Aeronautics and Space Administration, 1987.

Lachenbruch, Arthur H. Thermal measurements in Oak Springs Formation at the Nevada Test Site, southern Nevada. [Menlo Park, CA]: U.S. Geological Survey, 1987.

Gillespie, David. Temperature profiles and hydrologic implications from the Nevada Test Site Area. Las Vegas, NV: Desert Research Institute, 2005.

Kehoe, M. W. Thermoelastic vibration test techniques. Edwards, Calif: National Aeronautics and Space Administration, Ames Resarch Center, Dryden Flight Research Facility, 1991.

Kehoe, M. W. Thermoelastic vibration test techniques. Edwards, Calif: National Aeronautics and Space Administration, Ames Resarch Center, Dryden Flight Research Facility, 1991.

Anderson, Ken. Low temperature pavement performance: An evaluation using C-SHRP test road data. Ottawa: Transportation Association of Canada, 1999.

C, Moore Thomas. Recommended strain gage application procedures for various Langley Research Center balances and test articles. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Bigl, Susan R. Testing of materials from the Minnesota Cold Regions Pavement Research Test Facility. Hanover, NH: US Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1996.

Christensen, Donald W. Evaluation of indirect tensile test (IDT) procedures for low-temperature performance of hot mix asphalt. Washington, D.C: Transportation Research Board, 2004.

Könnecke, R. EC static high-temperature leach test: Summary report of a European Community interlaboratory round robin. Luxembourg: Commission of the European Communities, 1985.

Choi, Sung Rak. Dependency of shear strength on test rate in SiC/BSAS ceramic matrix composite at elevated temperature. [Cleveland, Ohio: NASA Glenn Research Center, 2003.

Bigl, Susan R. Modeling of Mn/ROAD test sections with the CRREL mechanistic pavement design procedure. Hanover, NH: U.S. Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1996.

Taylor, William J. Comparing the results of an analytical model of the no-vent fill process with no-vent fill test results for a 4.96 m℗đ (175 ft℗đ) tank. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Lewis, R. E. Geohydrologic data from a 4,403-foot geothermal test hole, Mountain Home Air Force Base, Elmore County, Idaho. Boise, Idaho: U.S. Geological Survey, 1988.

Lewis, R. E. Geohydrologic data from a 4,403-foot geothermal test hole, Mountain Home Air Force Base, Elmore County, Idaho. Boise, Idaho: U.S. Geological Survey, 1988.

Holt, JM, and PP Puzak, eds. Drop-Weight Test for Determination of Nil-Ductility Transition Temperature: User's Experience with ASTM Method E 208. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1986. http://dx.doi.org/10.1520/stp919-eb.

Geist, Jon. A water bath blackbody for the 5 to 60C̊ temperature range: Performance goal, design concept, and test results. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1986.

Geist, Jon. A water bath blackbody for the 5 to 60êC temperature range: Performance goal, design concept, and test results. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1986.

Geist, Jon. A water bath blackbody for the 5 to 60C̊ temperature range: Performance goal, design concept, and test results. Gaithersburg, Md: U.S. Dept. of Commerce, National Bureau of Standards, 1986.

Salerno, Louis J. Facility for interferometric testing of 1.25-m mirrors at liquid helium temperatures. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Zimmerman, Richard S. Strain energy release rate as a function of temperature and preloading history utilizing the edge delamination fatigue test method. [Washington, DC: National Aeronautics and Space Administration, 1989.

Haggett, R. D. Modification of the Gerin falling ball viscosity comparator model V3 for use at the standard test temperature of 100oC. Dartmouth, N.S: Defence Research Establishment Atlantic, 1989.

Mellina, Eric. Stream temperature response to clearcut logging in the central interior of British Columbia: Test of the predictive model developed by Mellina et al. (2002). Victoria: Pacific Forestry Centre, 2006.

Hendricks, Robert C. Brush seal performance and durability issues based on T-700 engine test results. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Ahmed, Rafiq. Design and test of low-profile composite aerospace tank dome: (MSFC Center Director's Discretionary Fund final report, project no. 96-28). [Marshall Space Flight Center], Ala: National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.

O'Mara, Duncan F. Effect of heating rate to test temperature on superplastic response in an A1-8%Mg-1%Li-0.2%Zr alloy. Monterey, California: Naval Postgraduate School, 1989.

Kopp, Robert William. Determination of the velocity, density, mass flux and enthalpy profiles for very high temperature arc jet nozzle flow. Monterey, Calif: Naval Postgraduate School, 1989.

Moran, Matthew E. Liquid Transfer Cryogenic Test Facility: Initial hydrogen and nitrogen no-vent fill data. [Washington, D.C.]: NASA, 1990.

Hillger, Donald W. Imager and sounder radiance and product validations for the GOES-12 science test. Washington, D.C: U.S. Dept. of Commerce, National Oceanic and Atmosperic Administration, National Environmental Satellite, Data, and Information Service, 2003.

Hillger, Donald W. Imager and sounder radiance and product validations for the GOES-12 science test. Washington, D.C: U.S. Dept. of Commerce, National Oceanic and Atmospheric Administration, National Environmental Satellite, Data, and Information Service, 2003.

Payne, Richard E. Air temperature shield tests. Woods Hole, Mass: Woods Hole Oceanographic Institution, 1987.

Woodall, K. B. ITER Task T332a (1995): Low-crygoenic [sic] distillation tests. Mississauga, Ont: Canadian Fusion Fuels Technology Project, 1996.

Wilkinson, C. High temperature cyclic behaviour of aerospace materials: room temperature validation tests of Ti-6Al-4V. Neuilly sur Seine, France: AGARD, 1994.

Institution, British Standards. Rubber- or plastics-coated fabrics: Low temperature tests. London: B.S.I., 1991.

Leeuwen, H. P. van. Automated measurement of crack length and load line displacement at elevated temperature. Neuilly sur Seine, France: AGARD, 1988.

Chato, David J. Ground testing for the no-vent fill of cryogenic tanks: Results of tests for a 71 cubic foot tank. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Hall, A. M. Summary report on elevated temperature tests for asbestos-free gasket materials. [Houston? Tex.]: National Association of Corrosion Engineers, 1990.

Vinson, Ted S., and D. H. Jung. Low-Temperature Cracking: Test Selection. National research council, 1994.

Baloh, Robert W. Hallpike’s Caloric Test. Oxford University Press, 2016. http://dx.doi.org/10.1093/med/9780190600129.003.0015.

V, Marshall B., and Roth Edward F, eds. Thermal measurements in Oak Springs Formation at the Nevada Test Site, southern Nevada. [Menlo Park, CA]: U.S. Geological Survey, 1987.

United States. National Aeronautics and Space Administration., ed. Test program, helium II, orbital resupply coupling: Final report. [Boulder, Colo.]: Ball Aerospace Systems Group, Ball Corp., 1991.

Passive orbital disconnect strut (PODS III) structural test program. Moffett Field, Calif: The Center, 1985.

Test program, helium II, orbital resupply coupling: Final report. [Boulder, Colo.]: Ball Aerospace Systems Group, Ball Corp., 1991.

United States. National Aeronautics and Space Administration., ed. High-temperature test facility at the NASA Lewis Engine Components Research Laboratory. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

United States. National Aeronautics and Space Administration., ed. High-temperature test facility at the NASA Lewis Engine Components Research Laboratory. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

United States. National Aeronautics and Space Administration., ed. High-temperature test facility at the NASA Lewis Engine Components Research Laboratory. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

C, Ehlers Robert, Parrott Edith, and United States. National Aeronautics and Space Administration., eds. NASA Lewis Research Center's Preheated Combustor and Materials Test Facility. [Washington, DC]: National Aeronautics and Space Administration, 1995.

NASA Lewis Research Center's Preheated Combustor and Materials Test Facility. [Washington, DC]: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. A test fixture for measuring high-temperature hypersonic-engine seal performance. [Washington, DC]: National Aeronautics and Space Administration, 1991.

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.