Books on the topic 'Tensile tests'

Center, Langley Research, ed. Manual for LDEF tensile tests. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

1935-, Adams Donald Frederick, and United States. National Aeronautics and Space Administration., eds. Static tensile and tensile creep testing of five ceramic fibers at elevated temperatures. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

F, Adams Donald, Zimmerman Richard S, and Ames Research Center, eds. Static tensile and tensile creep testing of four boron nitride coated ceramic fibers at elevated temperatures: Final report. Moffett Field, Calif: NASA Ames Research Center, 1989.

United States. National Aeronautics and Space Administration., ed. Rhenium material properties. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Center, Langley Research, ed. Baseline tensile tests of composite materials for LDEF exposure. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Poon, C. Tensile fracture of notched composite laminates. Ottawa, Ont: National Research Council Canada, 1991.

Ossa, William. Material characterization of superplastically formed titanium (Ti-6Al-2Sn-4Zr-2Mo) sheet. Hampton, Va: Langley Research Center, 1987.

Moore, Thomas J. Tensile strength of simulated and welded butt joints in W-Cu-composite sheet. Cleveland, Ohio: Lewis Research Center, 1994.

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Tensile creep and stress-rupture behavior of polymer derived SiC fibers. [Washington, DC]: National Aeronautics and Space Administration, 1994.

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Tensile creep and stress-rupture behavior of polymer derived SiC fibers. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Kindermann, M. R. A slow strain-rate tensile testing machine. Melbourne, Victoria: Dept. of Defence, Aeronautical Research Laboratory, 1989.

Center, Lewis Research, and United States. National Aeronautics and Space Administration., eds. High temperature mechanical characterization of ceramic matrix composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Man, Yun Hee, Goldsby Jon C, and United States. National Aeronautics and Space Administration., eds. Bend stress relaxation and tensile primary creep of a polycrystalline Ü-SiC fiber. [Washington, D.C: National Aeronautics and Space Administration, 1995.

C, Pauly Christopher, Pindera M. J. 1951-, and United States. National Aeronautics and Space Administration., eds. Experimental characterization and micromechanical modeling of woven carbon/copper composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1997.

R, Veazie David, Brinson L. Catherine, and Langley Research Center, eds. A comparison of tension and compression creep in a polymeric composite and the effects of physical aging on creep. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Center, Langley Research, ed. Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.

J. C. F. N. van Rijn. The use of composite fracture models to describe the blunt notch behaviour of metal laminates. Amsterdam: National Aerospace Laboratory, 1992.

P, Campion R., and United States. National Aeronautics and Space Administration., eds. Mechanical and physical properties of both unaged and aged Coflon and Tefzel: CAPP, international research project on the effects of chemical ageing of polymers on performance properties. Austin, Tex: Texas Research Institute, 1996.

P, Campion R., and United States. National Aeronautics and Space Administration., eds. Mechanical and physical properties of both unaged and aged Coflon and Tefzel: CAPP, international research project on the effects of chemical ageing of polymers on performance properties. Austin, Tex: Texas Research Institute, 1996.

K, Hill Eric v., and United States. National Aeronautics and Space Administration., eds. Characterization of longitudinal splitting and fiber breakage in Gr/Ep using acoustic emission data. [Washington, DC: National Aeronautics and Space Administration, 1993.

K, Hill Eric v., and United States. National Aeronautics and Space Administration., eds. Characterization of longitudinal splitting and fiber breakage in Gr/Ep using acoustic emission data. [Washington, DC: National Aeronautics and Space Administration, 1993.

A, DiCarlo James, and United States. National Aeronautics and Space Administration., eds. Thermomechanical behavior of advanced SiC fiber multifilament tows. [Washington, DC]: National Aeronautics and Space Administration, 1997.

United States. National Aeronautics and Space Administration., ed. "Creep of refractory fibers and modeling of metal and ceramic matrix composite creep behavior": (NCC-3-119), project closing report. [Washington, DC: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. Contamiantion [sic] removal using various solvents and methodologies: Final report. Brigham City, Utah: Morton Thiokol, Inc., Aerspace Group, Space Operations, 1989.

Garga. Effect of Hf-rich particles on the creep life of a high-strength NiAl single crystal alloy. [Washington, D.C: National Aeronautics and Space Administration, 1995.

E, Masters John, and Langley Research Center, eds. Standard methods for open hole tension testing of textile composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Moss, A. C. Fracture characteristics of carbon and aramis unidirectional composites in interlaminar shear and open hole tensile tests. Amsterdam: National Aerospace Laboratory, 1986.

P, Kaplar E., ed. Mechanical properties of unirradiated and irradiated Zr-1% Nb cladding: Procedures and results of low temperature biaxial burst tests and axial tensile tests. Washington, D.C: Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 2001.

P, Kaplar E., ed. Mechanical properties of unirradiated and irradiated Zr-1% Nb cladding: Procedures and results of low temperature biaxial burst tests and axial tensile tests. Washington, D.C: Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 2001.

United States. National Aeronautics and Space Administration., ed. An investigation of the loss of ductility in hydrogen charged Ý-Ti alloys: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. An investigation of the loss of ductility in hydrogen charged Ý-Ti alloys: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Instrumented impact and residual tensile strength testing of eight-ply carbon/epoxy specimens. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Whittenberger, J. Daniel. Elevated temperature creep properties of NiAl cryomilled with and without Y₂O₃. [Washington, D.C: National Aeronautics and Space Administration, 1995.

General Motors Research and Development Center. and United States. National Aeronautics and Space Administration., eds. Spitfire-1: A cooperative agreement for the development of rapid low-cost superplastic forming of aluminum : progress report, twelve-month deliverables, March 1, 1995-May 31, 1995. Warren, MI: The Center, 1995.

General Motors Research and Development Center. and United States. National Aeronautics and Space Administration., eds. Spitfire-1: A cooperative agreement for the development of rapid low-cost superplastic forming of aluminum : progress report, twelve-month deliverables, March 1, 1995-May 31, 1995. Warren, MI: The Center, 1995.

J, Biss Emily, and George C. Marshall Space Flight Center., eds. Low temperature mechanical testing of carbon-fiber/epoxy-resin composite materials. Marshall Space Flight Center, Ala: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1996.

Harris, C. E. Preliminary report on tests of tensile specimens with a part-through surface notch for a filament wound graphite/epoxy material. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

United States. National Aeronautics and Space Administration., ed. Microcracking in composite laminates under thermal and mechanical loading. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Masters, John E. Translaminar fracture toughness of a composite wing skin made of stitched warp-knit fabric: Under contract NAS1-96014. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Center, Langley Research, ed. Translaminar fracture toughness of a composite wing skin made of stitched warp-knit fabric: Under contract NAS1-96014. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.

S, Majumdar Bhaskar, and United States. National Aeronautics and Space Administration., eds. In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMC. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Gates, Thomas S. Time-dependent behavior of a graphite/thermoplastic composite and the effects of stress and physical aging. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Gates, Thomas S. Time dependent behavior of a graphite/thermoplastic composite and the effects of stress and physical aging. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Center, Langley Research, ed. Fracture testing of 2324-T39 aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Gates, Thomas S. Time-dependent behavior of a graphite/thermoplastic composite and the effects of stress and physical aging. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Gates, Thomas S. Time-dependent behavior of a graphite/thermoplastic composite and the effects of stress and physical aging. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Center, Langley Research, ed. Fracture testing of 2324-T39 aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

A, Setlock John, and United States. National Aeronautics and Space Administration., eds. Sapphire reinforced alumina matrix composites. [Washington, D.C: National Aeronautics and Space Administration, 1994.