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Books on the topic 'Tensile strength and elongation'

Author: Grafiati

Published: 3 June 2025

Last updated: 31 July 2025

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1

Serikov, Sergey. Impact on impact strength. INFRA-M Academic Publishing LLC., 2024. http://dx.doi.org/10.12737/2161513.

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The main purpose of the monograph is to identify the main patterns in assessing the operational reliability of metals on the basis of a mathematical model of unsteady deformation of an isotropic viscoplastic medium, with specified boundary, initial conditions and energy criterion of destruction. A physically based computational and experimental method for metal identification is formulated. Practical examples of the efficiency of the method for a wide class of materials are given: structural steels, titanium, aluminum and copper alloys. The assessment of the operational reliability of metals i

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2

Furter, R. Strength and elongation testing. Textile Institute, 1985.

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3

National Institute of Standards and Technology (U.S.), ed. Tensile strength of an interlocking composite connection. U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 2000.

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4

G, Ifju Peter, and Langley Research Center, eds. Through-the-thickness tensile strength of textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.

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5

G, Ifju Peter, and Langley Research Center, eds. Through-the-thickness tensile strength of textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.

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6

Carli, Charles G. Tensile and compressive MOE of flakeboards. U.S. Forest Service, 1988.

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7

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

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8

Kruenate, Jittiporn. Investigation of the tensile strength of crosslinked thermoplastic materials. UMIST, 1996.

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9

Showalter, K. L. Effect of length on tensile strength in structural lumber. U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1987.

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10

W, Green David, and Forest Products Laboratory (U.S.), eds. Moisture content and tensile strength of Douglas fir dimension lumber. U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1990.

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11

W, Green David, and Forest Products Laboratory (U.S.), eds. Moisture content and tensile strength of Douglas fir dimension lumber. U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1990.

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12

Center, Langley Research, and United States. National Aeronautics and Space Administration., eds. Synthesis and characterization of modified phenylethynyl terminated polyimides. National Aeronautics and Space Administration, Langley Research Center, 1998.

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13

Misir, Hemlata. Tensile strength of Otoform K2 silicon impression material: A comparative study. University College Northampton, 1999.

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14

Bansal, Narottam P. Effects of HF treatments on tensile strength of hi-nicalon fibers. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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15

1954-, Salpekar Satish A., United States. Army Aviation Research and Technology Activity., and Langley Research Center, eds. Scale effects on the transverse tensile strength of graphite epoxy composites. National Aeronautics and Space Administration, Langley Research Center, 1992.

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16

Bansal, Narottam P. Effects of HF treatments on tensile strength of hi-nicalon fibers. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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17

R, Wheeler Donald, Dickerson Robert M, and United States. National Aeronautics and Space Administration., eds. Tensile strength and microstructural characterization of uncoated and coated HPZ ceramic fibers. National Aeronautics and Space Administration, 1996.

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18

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

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19

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

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20

Gellman, Richard Evan. Muscle strain injury: An in vitro study of stretch rate dependence in elongation to failure. s.n.], 1991.

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21

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

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22

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). National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

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23

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). National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

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24

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

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25

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). National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

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26

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. National Aeronautics and Space Administration, 1994.

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27

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. National Aeronautics and Space Administration, 1994.

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28

A, DiCarlo James, and United States. National Aeronautics and Space Administration., eds. Time/temperature dependent tensile strength of SiC and Al₂O₃-based fibers. National Aeronautics and Space Administration, 1997.

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29

A, DiCarlo James, and United States. National Aeronautics and Space Administration., eds. Time/temperature dependent tensile strength of SiC and Al₂O₃-based fibers. National Aeronautics and Space Administration, 1997.

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30

A, DiCarlo James, and United States. National Aeronautics and Space Administration., eds. Time/temperature dependent tensile strength of SiC and Al₂O₃-based fibers. National Aeronautics and Space Administration, 1997.

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31

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. National Aeronautics and Space Administration, 1997.

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32

Institution, British Standards. British standard method for determination of breaking strength and elongation (strip method) of woven fabrics ... . B.S.I., 1986.

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33

Center, Langley Research, ed. Tensile behavior of tungsten and tungsten-alloy wires from 1300 to 1600 k. National Aeronautics and Space Administration, Lewis Research Center, 1988.

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34

Center, Langley Research, and United States. Army Aviation Systems Command., eds. Mechanical property characterization and impact resistance of selected graphite/PEEK composite materials. National Aeronautics and Space Administration, Langley Research Center, 1991.

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35

D, Kraitchman M., United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. Environmental effects on the tensile strength of chemically vapor deposited silicon carbide fibers. National Aeronautics and Space Administration, 1985.

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36

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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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37

Anita, Garg, Hull David R, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Microstructural and strength stability of a developmental CVD SiC fiber. National Aeronautics and Space Administration, 1995.

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38

Anita, Garg, Hull David R, United States. National Aeronautics and Space Administration., and U.S. Army Research Laboratory., eds. Microstructural and strength stability of a developmental CVD SiC fiber. National Aeronautics and Space Administration, 1995.

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39

A, Biaglow James, and United States. National Aeronautics and Space Administration., eds. Rhenium mechanical properties and joining technology. National Aeronautics and Space Administration, 1996.

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40

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. National Aeronautics and Space Administration, Langley Research Center, 1997.

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41

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. National Aeronautics and Space Administration, Langley Research Center, 1997.

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42

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. National Aeronautics and Space Administration, 1997.

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43

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

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44

Harrington, M. The torque test: A proposed new test to establish the tensile strength of concrete. Queen Mary and Westfield College, 1998.

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45

Kevin, O'Brien T., and Langley Research Center, eds. Influence of specimen preparation and specimen size on composite transverse tensile strength and scatter. National Aeronautics and Space Administration, Langley Research Center, 2001.

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46

Center, Langley Research, ed. Test methods for textile composites. National Aeronautics and Space Administration, Langley Research Center, 1994.

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47

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

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48

Center, Langley Research, ed. Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate. National Aeronautics and Space Administration, Langley Research Center, 1990.

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49

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

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50

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. National Aeronautics and Space Administration, 1995.

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