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Ti-6Al-4V

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Published: 01 October 2012
Fig. 5.33 Fracture toughness of Ti-6Al-4V castings compared with that of Ti-6Al-4V plate and other titanium alloys. Source: Ref 5.4 More
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Published: 01 February 2005
Fig. 20.8 Flow stress data for Ti-10V-2Fe-Al compared with that of Ti-6Al-4V [ Rosenberg, 1978 ] More
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Published: 01 November 2012
Fig. 50 Notch effects on (a) Ti-6Al-4V and (b) Ti-10V-2Fe-3Al. Source: Ref 30 , 31 More
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Published: 01 January 2015
Fig. 6.9 Effect of section size on tensile properties of Ti-6Al-4V and Ti-13V-11Cr-3Al. A is 788 °C (1450 °F) 30 min water quenched; 482 °C (900 °F) 48 h air cooled. B is 927 °C (1700 °F) 1 h water quenched; 482 °C (900 °F) 6 h air cooled. Courtesy of Titanium Metal Corp. of America More
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Published: 01 December 2000
Fig. 12.47 Young’s modulus for Ti-5Al-2.5Sn and Ti-6Al-4V alloys versus temperature in the low-temperature region More
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Published: 01 December 2000
Fig. 12.48 Poisson’s ratio for Ti-5Al-2.5Sn and Ti-6Al-4V alloys versus temperature in the low-temperature region More
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Published: 01 December 2000
Fig. 12.49 Fatigue crack propagation rates for Ti-5Al-2.5Sn and Ti-6Al-4V alloys in the low-temperature region. NI = normal interstitial content; ELI = extra low interstitial content More
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Published: 01 February 2005
Fig. 20.2 Comparison between conventional and hot-die forging of a Ti-6Al-4V structural part on the basis of raw material saved [ Shah, 1988 ] More
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Published: 01 June 2016
Fig. 11.12 (a and b) Optimization of cold-sprayed titanium on the Ti-6Al-4V chafing tubing repair by using different types of powders. (b) Bond adhesion strength of the different powders. (c) Coating microstructure comparison between helium and nitrogen process gas. (d) Various cold spray More
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Published: 01 June 2016
Fig. 11.12 (a and b) Optimization of cold-sprayed titanium on the Ti-6Al-4V chafing tubing repair by using different types of powders. (b) Bond adhesion strength of the different powders. (c) Coating microstructure comparison between helium and nitrogen process gas. (d) Various cold spray More
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Published: 01 December 2015
Fig. 21 Micrograph showing cracking of sectioned alloy Ti-6Al-4V fatigue specimen prefretted before fatigue testing. Arrows indicate branching crystallographic cracks. More
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Published: 01 December 2015
Fig. 23 Corrosion fatigue of a Ti-6Al-4V alloy tested in ambient air. Intergranular cracking and fatigue striations are evident on the fracture surface; the grain appears to have separated from the rest of the microstructure. Source: Ref 21 More
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Published: 01 October 2011
Fig. 14.28 Effect of solution treatment on tensile properties of Ti-6Al-4V. (a) Tensile properties after solution treatment. (b) Tensile properties after solution treatment and aging. Source: Ref 14.10 More
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Published: 01 June 2008
Fig. 28.7 Ti-6Al-4V microstructures produced by cooling from different temperatures. Original magnification: 250×. Source: Ref 1 More
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Published: 01 June 2008
Fig. 28.12 Effects of thermomechanical processing on microstructure of Ti-6Al-4V. (a) Sheet, rolled starting at 925 °C (1700 °F), annealed for 8 h at 730 °C (1350 °F), and furnace cooled. Structure consists of slightly elongated grains of alpha (light) and intergranular beta (gray). Original More
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Published: 01 June 2008
Fig. 28.13 Effect of hot isostatic pressing (HIP) on fatigue properties of Ti-6Al-4V investment castings. Room temperature smooth bar, tension-tension fatigue, R = +0.1 Source: Ref 2 More
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Published: 01 June 2008
Fig. 28.14 Effect of solution heat treating temperature on Ti-6Al-4V sheet More
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Published: 01 January 2000
Fig. 53 Stress-corrosion failure of an Apollo Ti-6Al-4V RCS pressure vessel due to nitrogen tetroxide. (a) Failed vessel after exposure to pressurized N 2 O 4 for 34 h. (b) Cross section through typical stress-corrosion cracks. 250× More
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Published: 01 January 2017
Fig. 10.5 Range of K IC and K ISCC values for Ti-6Al-4V in various metallurgical conditions in 3.5% NaCl solution at 24 °C (75 °F). Source: Ref 10.4 More
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Published: 01 January 2017
Fig. 10.26 Stress cracking depth on a (STA) Ti-6Al-4V sample stressed in tension and in bearing contact with solid cadmium for various temperatures and times. Source: Ref 10.74 More