[PDF] Review Of Current Data On The Tensile Properties Of Metals At Very Low Temperatures eBook

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Low Temperature Properties of Selected Materials

Author : Dorothea M. Johnson
Publisher :
Page : 182 pages
File Size : 26,36 MB
Release : 1977
Category : Low temperatures
ISBN :

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This report is a bibliography of the work reported in the literature on the effects of low temperature on the properties of structural materials. Some of the newer areas of cryogenic technology such as superconducting machinery involve environments which may subject the components to temperature as low as 4 K. Exposure of structural materials to such low temperatures affects their properties. This bibliography contains 963 references published between 1950-1976, arranged in chronological/alphabetical order. Combined material/property indexes are provided. (Author).

Properties of Aluminum Alloys

Author : John Gilbert Kaufman
Publisher : ASM International
Page : 332 pages
File Size : 49,84 MB
Release : 1999-01-01
Category : Technology & Engineering
ISBN : 9780871706324

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A compilation of data collected and maintained for many years as the property of a large aluminum company, which decided in 1997 to make it available to other engineers and materials specialists. In tabular form, presents data on the tensile and creep properties of eight species of wrought alloys and five species of cast alloys in the various shapes used in applications. Then looks at the fatigue data for several alloys under a range of conditions and loads. The data represent the typical or average findings, and though some were developed years ago, the collection is the largest and most detailed available. There is no index.

Statistical Analysis of Tensile Properties of Heat-treated Ti-4A1-3Mo-1V and Ti-2.5A1-16V Sheet

Author : G. H Beatty
Publisher :
Page : 54 pages
File Size : 10,82 MB
Release : 1961
Category : Metals
ISBN :

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IN THE SOLUTION TREATED AND AGED CONDITION, Ti4Al-3Mo-1V has a higher ultimate strength than does Ti-2.5Al-16V, but the two alloys are about even in yield strength and elongation. In the solution-treated condition, Ti-4Al-3Mo-1V is unquestionably stronger than Ti-2.5Al-16V. These conclusions are independent of producer. There is not much difference in the same alloy produced by different companies. The alloys developed under the Titanium-Alloy Sheet-Rolling Program would not endure the most critical interpretation of release property specifications. On the other hand, these alloys come reasonably close to specifications. A complete set of release property specifications is available only for specimens that have been solution treated and aged. Such specimens do not all exhibit the desired ultimate and yield strength, but the percentage of rejects is small enough to be encouraging. (Author).

Refrigeration Engineering

Author :
Publisher :
Page : 876 pages
File Size : 48,93 MB
Release : 1942
Category :
ISBN :

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English abstracts from Kholodil'naia tekhnika.