Stress-corrosion Failure in high strength aluminium-zinc-magnesium alloys

Stress-corrosion Failure in high strength aluminium-zinc-magnesium alloys PDF Author: Robin Shipp
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Category :
Languages : en
Pages :

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Stress-corrosion Cracking in High Strength Steels and in Titanium and Aluminum Alloys

Stress-corrosion Cracking in High Strength Steels and in Titanium and Aluminum Alloys PDF Author: Benjamin Floyd Brown
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ISBN:
Category : Aluminum alloys
Languages : en
Pages : 388

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Stress-corrosion Cracking of Aluminum Alloys

Stress-corrosion Cracking of Aluminum Alloys PDF Author: F. H. Haynie
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Category : Aluminum alloys
Languages : en
Pages : 52

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This report deals with the stress-corrosion cracking of aluminum alloys, and it represents an effort by DMIC to expand on the information contained in DMIC Memorandum 202, 'Stress-Corrosion Cracking of Aluminum Alloys', dated February 15, 1965. DMIC Report 228 begins by presenting a comprehensive definition of stress-corrosion cracking. This is followed by sections dealing with (1) the historical development and growth in awareness of the problem, (2) the mechanisms involved, and (3) the theory of stress-corrosion cracking. A section on experimental techniques is presented. These techniques include test methods used to determine the susceptibility of alloys to stress-corrosion cracking, as well as more refined methods of studying the fundamental mechanisms of the problem. Different evaluation methods, applicable to obtaining the different objectives of stress-corrosion testing, are also presented. All of the foregoing serve as background to the sections on stress-corrosion-cracking behavior of aluminum alloys and preventive measures. (Author).

Mechanism of Stress Corrosion Cracking in Medium Strength Aluminium-zinc-magnesium Alloy System

Mechanism of Stress Corrosion Cracking in Medium Strength Aluminium-zinc-magnesium Alloy System PDF Author: M. L. Mehta
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Category : Alloys
Languages : en
Pages :

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Aluminium-zinc-magnesium Alloys, with Special Reference to Their Failure by Stress-corrosion

Aluminium-zinc-magnesium Alloys, with Special Reference to Their Failure by Stress-corrosion PDF Author: Henry Jeffrey Blewden
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Category :
Languages : en
Pages : 0

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The Stress Corrosion of Metals

The Stress Corrosion of Metals PDF Author: Hugh Lynn Logan
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Category : Technology & Engineering
Languages : en
Pages : 328

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The Constitution, Stress-corrosion and Other Properties of High Strength Aluminium Alloys Containing Magnesium and Zinc

The Constitution, Stress-corrosion and Other Properties of High Strength Aluminium Alloys Containing Magnesium and Zinc PDF Author: B. T. Houlden
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Languages : en
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The Development Of Aluminium -zinc- Magnesium Alloys For Superior Stress Corrosion Resistance

The Development Of Aluminium -zinc- Magnesium Alloys For Superior Stress Corrosion Resistance PDF Author: Dauskardt Reinhold Horst
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Category :
Languages : en
Pages : 412

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Stress Corrosion Cracking of Welded Aluminium-zinc-magnesium Alloys

Stress Corrosion Cracking of Welded Aluminium-zinc-magnesium Alloys PDF Author: Simon Richard Tracey
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Category : Aluminum-magnesium-zinc alloys
Languages : en
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Stress-Corrosion Cracking of High-Strength Aluminum Alloys

Stress-Corrosion Cracking of High-Strength Aluminum Alloys PDF Author: E. N. Pugh
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Category :
Languages : en
Pages : 13

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A study has been made of the mechanism of hydrogen embrittlement (HE) in Al-Zn-Mg alloys, and of the role of hydrogen in the intergranular stress-corrosion cracking (I-SCC) of these alloys. Up to 300 ppm (1 at pct) hydrogen was introduced into a high-purity Al-5.6Zn-2.6Mg alloy, either by room temperature polishing with aqueous slurries of alumina particles or by exposure to water-vapor-saturated air (WVSA) at 70 C, and subsequent tensile tests (stress rate approx 0.0001/s) in inert environments caused brittle intergranular fracture. Embrittlement was found to be reversible, the tensile properties being completely restored when the hydrogen was outgassed. At low hydrogen contents, embrittlement was suppressed by the use of high strain rates (approx 0.01/s), but could not be suppressed by impact testing at large hydrogen concentrations. The intergranular fracture surfaces were observed to be associated with a fragmented layer, and electron-diffraction experiments indicated that it corresponded to a hexagonal aluminum hydride, Al H3, with a = 2.90 A and c = 4.55 A. This hydride, considered to be stress-induced, was unstable in laboratory air, slowly decomposing to FCC Al. It is concluded that internal HE in this alloy occurs by repeated cycles of the formation and rupture of this brittle hydride.