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1

J, Fields R., and National Institute of Standards and Technology (U.S.), eds. A computer-controlled tensile stage for in-situ X-ray measurements. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1997.

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2

J, Fields R., and National Institute of Standards and Technology (U.S.), eds. A computer-controlled tensile stage for in-situ X-ray measurements. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1997.

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3

J, Fields R., and National Institute of Standards and Technology (U.S.), eds. A computer-controlled tensile stage for in-situ X-ray measurements. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1997.

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4

J, Fields R., and National Institute of Standards and Technology (U.S.), eds. A computer-controlled tensile stage for in-situ X-ray measurements. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1997.

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5

J, Fields R., and National Institute of Standards and Technology (U.S.), eds. A computer-controlled tensile stage for in-situ X-ray measurements. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1997.

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6

J, Fields R., and National Institute of Standards and Technology (U.S.), eds. A computer-controlled tensile stage for in-situ X-ray measurements. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1997.

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7

J, Fields R., and National Institute of Standards and Technology (U.S.), eds. A computer-controlled tensile stage for in-situ X-ray measurements. Gaithersburg, MD: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1997.

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8

Center, Lewis Research, ed. Modfications of system for elevated temperature testing and stress-strain measurement of metal matrix composites. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

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9

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

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10

Alex, Vary, and United States. National Aeronautics and Space Administration., eds. Tensile strain measurements of ceramic fibers using scanning laser acoustic microscopy. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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11

A, Williams. Tests on large reinforced concrete elements subjected to direct tension. Wexham Springs: Cement and Concrete Association, 1986.

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12

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.

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13

Dutta, Piyush K. High-strain-rate tensile behavior of sedimentary and igneous rocks at low temperatures. [Hanover, N.H.]: U.S. Army Corps of Engineers, Cold Regions Research & Engineering Laboratory, 1993.

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14

F, Erdogan, and Langley Research Center, eds. The surface crack problem in an orthotropic plate under bending and tension. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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15

M, Arnold S., and NASA Glenn Research Center, eds. An analysis of the macroscopic tensile behavior of a nonlinear nylon reinforced elastomeric composite system using MAC/GMC. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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16

1963-, Terry Angela M., and Forest Products Laboratory (U.S.), eds. Gripped-end effect in tension proof testing of dimension lumber. Madison, WI: U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1991.

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17

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

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18

S, Piascik Robert, and Langley Research Center, eds. A back face strain compliance expression for the compact tension specimen. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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19

Huddleston, John V. Extensiblity and compressibiity in one-dimensional structures: Cables, tension rods, compression rods, frames, and arches. Buffalo, N.Y., U.S.A: Exchange Pub. Div., 1993.

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20

Huddleston, John V. Extensibility and compressibility in one-dimensional structures: Cables, tension rods, compression rods, frames, arches, and rings. 2nd ed. Buffalo, N.Y: Exchange Pub. Division, 2000.

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21

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.

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22

Mabson, Gerald E. Analysis and testing of composite aircraft frames for interlaminar tension failure. [S.l.]: [s.n.], 1988.

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23

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.

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24

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.

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25

Naik, Rajiv A. Failure analysis of woven and braided fabric reinforced composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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26

Naik, Rajiv A. Failure analysis of woven and braided fabric reinforced composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

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27

S, Raju I., O'Brien T. Kevin, Langley Research Center, and United States. Army Aviation Research and Technology Activity., eds. Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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28

Floyd, Esme. Body massage: [the at-home massage class to release tension, relieve muscle strain and recover after sport]. London: Carlton Books, 2010.

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29

Alfred, Buch. Prediction of constant-amplitude fatigue life to failure under pulsating-tension by use of the local-strain-approach. Haifa: Technion Israel Institute of Technology, 1989.

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30

Alfred, Buch. Prediction of constant-amplitude fatigue life to failure under pulsating-tension (R > 0) by use of the local-strain-approach. Haifa, Israel: Technion - Israel Institute of Technology, Faculty of Aerospace Engineering, 1991.

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31

United States. National Aeronautics and Space Administration., ed. Creep and stress relaxaton modeling of polycrystalline ceramic fibers. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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32

Andy, Resnik, Kaukler William F, and United States. National Aeronautics and Space Administration., eds. Stability limits and dynamics of nonaxisymmetric liquid bridges: First annual report ... Huntsville, Ala: Center for Microgravity and Materials Research, University of Alabama in Huntsville, 1993.

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33

Schindler, Paul. Optical fiber sensors for damage analysis in aerospace materials: Final report. [Washington, D.C: National Aeronautics and Space Administration, 1995.

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34

Sanders, J. Oswald. Overcoming Tension and Strain. O M F Books, 1987.

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35

Davis, J. R., ed. Tensile Testing. 2nd ed. ASM International, 2004. http://dx.doi.org/10.31399/asm.tb.tt2.9781627083553.

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Abstract:
Tensile Testing, Second Edition is a comprehensive guide to the uniaxial tensile test and its use in determining the mechanical properties and behaviors of materials. The first six chapters cover the fundamentals of tensile testing, including the methodology, the equipment used, the effect of tensile loading on metals, the interpretation of data, and the role of tensile testing in design and manufacturing. The next six chapters deal with the testing of different classes of engineering materials, namely metals, plastics, elastomers, ceramics, and composites, and fabricated structures such as weldments and bolted and adhesively bonded joints. The book also includes three chapters on the nuances of tensile testing at extreme temperatures and strain rates and a reference section with data tables. For information on the print version, ISBN 978-0-87170-806-9, follow this link.
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36

Optical strain measuring techniques for high temperature tensile testing. [Cleveland, Ohio]: National Aeronautics and Space Administration, 1987.

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37

Wire Ropes: Tension, Endurance, Reliability. Springer, 2007.

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38

Feyrer, Klaus. Wire Ropes: Tension, Endurance, Reliability. Springer, 2014.

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39

Feyrer, Klaus. Wire Ropes: Tension, Endurance, Reliability. Springer, 2014.

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40

Feyrer, Klaus. Wire Ropes: Tension, Endurance, Reliability. Springer, 2010.

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41

Feyrer, Klaus. Wire Ropes: Tension, Endurance, Reliability. Springer, 2014.

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42

Feyrer, Klaus. Wire Ropes: Tension, Endurance, Reliability. Springer London, Limited, 2007.

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43

An analysis of the macroscopic tensile behavior of a nonlinear nylon reinforced elastomeric composite system using MAC/GMC. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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44

A back face strain compliance expression for the compact tension specimen. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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45

Huddleston, John V. Extensibility and Compressibility in One-Dimensional Structures: Cables, Tension Rods, Compression Rods, Frames, and Arches. Exchange Pub Division, 1993.

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46

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.

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47

Dynamic Tensile Testing of Sheet Steels and Influence of Strain Rate on Strengthening Mechanisms in Sheet Steels. Storming Media, 2003.

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48

Hewett, Delane Robert. An application of computer-aided analysis for the study of stretch forming in uniaxial tension. 1986.

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49

Property evaluation of LTM25 composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

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50

Strength scaling in fiber composites. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1990.

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