Author: Howard L. PricePublisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
Tensile Properties of 6Al-4V Titanium-alloy Sheet Under Rapid-heating and Constant-temperature Conditions
Author: Howard L. PriceTensile Properties of 6A1-4V Titanium-alloy Sheet Under Rapid-heatiing and Constant-temperature Conditions
Author: Howard L. PricePublisher:
ISBN:
Category : Alloys
Languages : en
Pages : 30
Book Description
Tensile Properties of 6A1-4V Titanium-alloy Sheet Under Rapid-heatiing and Constant-temperature Conditions
Author: Howard L. PricePublisher:
ISBN:
Category : Alloys
Languages : en
Pages : 26
Book Description
Tensile Properties of Inconel and RS-120 Titanium-alloy Sheet Under Rapid-heating and Constant-temperature Conditions
Author: George J. HeimerlPublisher:
ISBN:
Category : Inconel
Languages : en
Pages : 29
Book Description
Results are presented of rapid-heating tests to deternine the tensile strength of lnconel and RS-120 titanium-alloy sheet heated to failure at uniform temperature rates from 0.2 F to 100 degrees F per second under constant load condltions. Yield and rupture stresses, obtained by rapid heating, are compared with yield and ultimate stresses from elevated-temperature tensile stress-strain tests for 1/2-hour exposure. The applicability of master curves and temperature-rate parameters to the prediction of yield and rupture stresses and temperatures under rapid-heating conditions was investigated.
Statistical Analysis of Tensile Properties of Heat-treated Ti-4A1-3Mo-1V and Ti-2.5A1-16V Sheet
Author: G. H BeattyPublisher:
ISBN:
Category : Metals
Languages : en
Pages : 54
Book Description
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).
Nuclear Science Abstracts
Author: Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1812
Book Description
Index of N A S A Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages : 498
Book Description
Smooth and Sharpe-notch Property Variations for Several Heats of Ti-6A1-4V Sheet at Room and Cryogenic Temperatures
Author: Morgan P. HansonPublisher:
ISBN:
Category : Statistical matching
Languages : en
Pages : 22
Book Description
Author: