Books on the topic 'TENSILE PROPERTIES'

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

Erdogan, M. Bauschinger annd tensile properties of dual phase steels. Manchester: UMIST, 1993.

Wood, D. S. The tensile properties of austenitic steel weld metals. Luxembourg: Commission of the European Communities, 1986.

T, Herakovich Carl, Sykes George F, and Langley Research Center. Applied Materials Branch., eds. Space environmental effects on graphite-epoxy compressive properties and epoxy tensile properties. Hampton, VA: Applied Materials Branch, National Aeronautics and Space Administration, Langley Research Center, 1987.

Billinghurst, E. E. Tensile properties of cast titanium alloys: Titanium-6A1-4V ELI and Titanium-5Al-2.5Sn ELI. Huntsville, Ala: George C. Marshall Space Flight Center, 1992.

England), Textile Institute (Manchester, ed. Handbook of tensile properties of textile and technical fibres. Cambridge, UK: Woodhead Publishing in association with the Textile Institute, 2009.

Nieuwland, H. C. D. Comparison of the tensile properties of 9-12% CR. Steels. Luxembourg: Commission of the European Communities, 1985.

Center, Lewis Research, ed. Tensile properties and microstructural characterization of Hi-Nicalon SiC/RBSN composites. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

F, Van Bramer Thomas, and New York (State). Engineering Research and Development Bureau, eds. Resilient and tensile properties of New York State asphalt concrete mixes. Albany, N.Y: Engineering Research and Development Bureau, New York State Dept. of Transportation, 1990.

A, Biaglow James, and United States. National Aeronautics and Space Administration., eds. Rhenium mechanical properties and joining technology. [Washington, D.C: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Tensile properties of cast titanium alloys: Titanium-6Al-4V ELI and Titanium-5Al-2.5Sn ELI. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Tensile properties of cast titanium alloys: Titanium-6Al-4V ELI and Titanium-5Al-2.5Sn ELI. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 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.

Fong, Randy W. L., 1954- and Chalk River Laboratories, eds. Tensile properties of irradiated calandria tubes at low to high rates of strain. [Chalk River, Ont: Chalk River Laboratories], 1997.

P, Gabb Timothy, and NASA Glenn Research Center, eds. The tensile properties of advanced nickel-base disk superalloys during quenching heat treatments. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

A, DiCarlo James, and NASA Glenn Research Center, eds. Comparison of the tensile, creep, and rupture strength properties of stoichiometric SiC fibers. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Long, Edward R. Spectroscopic analysis of radiation-generated changes in tensile properties of a polyetherimide film. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Bhatt, Ramakrishna T. Microstructure and tensile properties of BN/SiC coated Hi-Nicalon, and Sylramic SiC fiber preforms. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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.

Raj, Subramanium Varada. Modeling the role of dislocation substructure during class M and exponential creep. [Washington, DC]: National Aeronautics and Space Administration, 1995.

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.

1952-, Saleeb Atef F., Castelli Michael G, and United States. National Aeronautics and Space Administration., eds. A fully associative, nonisothermal, nonlinear kinematic, unified viscoplastic model for titanium alloys. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

George C. Marshall Space Flight Center., ed. High-strength aluminum casting alloy for high-temperature applications: (MSFC Center director's discretionary fund final project no. 97-10). [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

George C. Marshall Space Flight Center., ed. High-strength aluminum casting alloy for high-temperature applications: (MSFC Center director's discretionary fund final project no. 97-10). [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

Lee, J. A. High-strength aluminum casting alloy for high-temperature applications: (MSFC Center director's discretionary fund final project no. 97-10). [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

George C. Marshall Space Flight Center., ed. High-strength aluminum casting alloy for high-temperature applications: (MSFC Center director's discretionary fund final project no. 97-10). [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Effects of thermal treatment on tensile creep and stress-rupture behavior on Hi-Nicalon SiC fibers. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration. and U.S. Army Research Laboratory., eds. Heat treatment effects on the tensile properties and microstructures of a SiC/RBSN composite in nitrogen. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

D, Kiser James, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. Matrix density effects on the mechanical properties of SiC/RBSN composites. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

M, Fisher Douglas, and Lewis Research Center, eds. Influence of fatigue crack wake length and state of stress and on crack closure. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

L, Norman Timothy, and Langley Research Center, eds. Effect of open hole on tensile failure properties of 2D triaxial braided textile composites and tape equivalents. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Larry, Sobel, and Langley Research Center, eds. Novel composites for wing and fuselage applications: Speedy Nonlinear Analysis of Postbuckled Panels in Shear (SNAPPS) : under contract NAS1-18784. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Larry, Sobel, and Langley Research Center, eds. Novel composites for wing and fuselage applications: Speedy Nonlinear Analysis of Postbuckled Panels in Shear (SNAPPS) : under contract NAS1-18784. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Long, Edward R. Spectroscopic comparison of effects of electron radiation on mechanical properties of two polyimides. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

C, Newman J., and Langley Research Center, eds. Analyses of buckling and stable tearing in thin-sheet materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Bind, A. K. Mechanical properties of Zr-2.5Nb pressure tube material manufactured employing forging routes for PHWR700 - Part I: Tensile behaviour. Mumbai: Scientific Information Resource Division, Bhabha Atomic Research Centre, 2012.

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.

Bakis, Charles E. Fatigue response of notched laminates subjected to tension-compression cyclic loads. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1986.

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

United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. Effects of chromium and aluminum on mechanical and oxidation properties of iron-nickel-base superalloys based on CG-27. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Chadwick, H. The effect of compositional changes on the hot-shortness and tensile properties of the high strength aluminium casting alloy K0-1. Birmingham: University of Birmingham, 1992.

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.

M, Yun H., DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Creep and rupture strength of an advanced CVD SiC fiber. [Washington, DC]: National Aeronautics and Space Administration, 1997.

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.

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.

1938-, Gyekenyesi John P., Bhatt Ramakrishna T, and Lewis Research Center, eds. Mechanical behavior of fiber reinforced SiC/RBSN ceramic matrix composites: Theory and experiment. [Cleveland, Ohio: Lewis Research Center, 1991.

1938-, Gyekenyesi John P., Bhatt Ramakrishna T, and Lewis Research Center, eds. Mechanical behavior of fiber reinforced SiC/RBSN ceramic matrix composites: Theory and experiment. [Cleveland, Ohio: Lewis Research Center, 1991.

Schiess, James R. Two algorithms for rational spline interpolation of surfaces. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.