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Published: 30 November 2013
Fig. 1 Elastic stress distribution: pure tension. T, tension. C, compression. (a) No stress concentration. (b) Surface stress concentrations. (c) Transverse hole stress concentration More
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Published: 01 December 2003
Fig. 21 Examples of translaminar tension fractures. (a) Translaminar tension fracture in a graphite/epoxy composite. Note fiber bundles and individual fiber pullout. 400×. Source: Ref 2 . (b) Translaminar tension failure with localized area of flat fracture. 2000×. Source: Ref 2 . (c) Radial More
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Published: 01 March 2006
Fig. 12.8 Monotonic tension and cyclic tension and compression stress-strain curves for polycarbonate at room temperature. Source: Ref 12.4 More
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Published: 30 November 2013
Fig. 3 Elastic stress distribution: pure compression. T, tension. C, compression. (a) No stress concentration. (b) Surface stress concentrations. (c) Transverse hole stress concentration More
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Published: 30 November 2013
Fig. 4 Elastic stress distribution: pure bending. T, tension. C, compression. (a) No stress concentration. (b) Transverse surface stress concentrations More
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Published: 30 November 2013
Fig. 5 Elastic stress distribution: interference fit (press or shrink). T, tension. C, compression. More
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Published: 30 November 2013
Fig. 1 Schematic tension-creep curve, showing the three stages of creep. Source: Ref 4 More
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Published: 30 November 2013
Fig. 2 Creep curves for a molybdenum-vanadium low-alloy steel under tension at four stress levels at 600 °C (1112 °F). Source: Ref 2 More
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Published: 30 November 2013
Fig. 3 Modes of loading. Mode I (opening mode): tension stress in the y direction, or perpendicular to crack surfaces. Mode II (edge-sliding mode): shear stress in the x direction, or perpendicular to the crack tip. Mode III (tearing mode): shear stress in the z direction, or parallel More
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Published: 01 June 2008
Fig. 2.24 Tension loading of single and polycrystalline metals More
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Published: 01 November 2011
Fig. 9.7 The four basic types of adhesive loading. Tension and shear are acceptable loading methods, provided the bond area is sufficient. Cleavage and peel are to be avoided. More
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Published: 01 December 2004
Fig. A3.7 Compact tension plane strain fracture toughness specimen. Refer to ASTM E 399. More
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Published: 01 December 2004
Fig. 6 Example of the Bauschinger effect and hysteresis loop in tension-compression-tension loading. This example shows initial tension loading to 1% strain, followed by compression loading to 1% strain, and then a second tension loading to 1% strain. More
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Published: 01 December 2004
Fig. 1 Bar under axial tension More
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Published: 01 December 2004
Fig. 4 Typical tension failure of multidirectional laminate using a tabbed coupon More
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Published: 01 December 2004
Fig. 3 Torque-tension research head, 800 kN capacity More
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Published: 01 December 2004
Fig. 16 Specimen for testing cleavage peel (by tension loading). Source: ASTM D 3807 More
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Published: 01 December 2004
Fig. 1 Gleeble test unit used for hot-tension and hot-compression testing. (a) Specimen in grips showing attached thermocouple wires and linear variable differential transformer (LVDT) for measuring strain. (b) Close-up of a test specimen. Courtesy of Duffers Scientific, Inc. More
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Published: 01 December 2004
Fig. 14 True-stress/true-strain data for an Al-8090 alloy deformed in tension at 520 °C (970 °F) and a true strain rate of 7.8 × 10 –4 s –1 . Source: Ref 16 More
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Published: 01 December 2004
Fig. 31 Micrographs of titanium aluminide specimens that failed in tension. (a) Orthorhombic titanium aluminide that failed in tension by flow localization. Source: Ref 10 . (b) Near-γ titanium aluminide that failed in tension by fracture (cavitation). Source: Ref 51 More