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Analytic Model of Maximal Experimental Value of Stress Intensity Factor K(Q) for AA2519–AA1050–Ti6Al4V Layered Material

The article presents the results of the author’s tests involving the determination of the maximal experimental value of the stress intensity factor K(Q). This value was determined for a layered material obtained as the result of explosive welding of three alloys: AA2519, Ti6Al4V and AA1050, and sepa...

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Autor principal: Kotyk, Maciej
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7579026/
https://www.ncbi.nlm.nih.gov/pubmed/33036246
http://dx.doi.org/10.3390/ma13194439
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author Kotyk, Maciej
author_facet Kotyk, Maciej
author_sort Kotyk, Maciej
collection PubMed
description The article presents the results of the author’s tests involving the determination of the maximal experimental value of the stress intensity factor K(Q). This value was determined for a layered material obtained as the result of explosive welding of three alloys: AA2519, Ti6Al4V and AA1050, and separately for each material. In both cases tests were conducted for two temperatures—the ambient temperature (293 K), and cryogenic temperature (77 K). A model for initial assessment of the K(Q) value of AA2519–AA1050–Ti6Al4V (Al–Ti) layered material has also been presented. The proposed model has been developed so as to enable the determination of the curve course of load–COD for Al–Ti layered material using nominal stresses defined on the basis of a real load–COD course, obtained for the base materials, for both temperature conditions.
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spelling pubmed-75790262020-10-29 Analytic Model of Maximal Experimental Value of Stress Intensity Factor K(Q) for AA2519–AA1050–Ti6Al4V Layered Material Kotyk, Maciej Materials (Basel) Article The article presents the results of the author’s tests involving the determination of the maximal experimental value of the stress intensity factor K(Q). This value was determined for a layered material obtained as the result of explosive welding of three alloys: AA2519, Ti6Al4V and AA1050, and separately for each material. In both cases tests were conducted for two temperatures—the ambient temperature (293 K), and cryogenic temperature (77 K). A model for initial assessment of the K(Q) value of AA2519–AA1050–Ti6Al4V (Al–Ti) layered material has also been presented. The proposed model has been developed so as to enable the determination of the curve course of load–COD for Al–Ti layered material using nominal stresses defined on the basis of a real load–COD course, obtained for the base materials, for both temperature conditions. MDPI 2020-10-06 /pmc/articles/PMC7579026/ /pubmed/33036246 http://dx.doi.org/10.3390/ma13194439 Text en © 2020 by the author. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).
spellingShingle Article
Kotyk, Maciej
Analytic Model of Maximal Experimental Value of Stress Intensity Factor K(Q) for AA2519–AA1050–Ti6Al4V Layered Material
title Analytic Model of Maximal Experimental Value of Stress Intensity Factor K(Q) for AA2519–AA1050–Ti6Al4V Layered Material
title_full Analytic Model of Maximal Experimental Value of Stress Intensity Factor K(Q) for AA2519–AA1050–Ti6Al4V Layered Material
title_fullStr Analytic Model of Maximal Experimental Value of Stress Intensity Factor K(Q) for AA2519–AA1050–Ti6Al4V Layered Material
title_full_unstemmed Analytic Model of Maximal Experimental Value of Stress Intensity Factor K(Q) for AA2519–AA1050–Ti6Al4V Layered Material
title_short Analytic Model of Maximal Experimental Value of Stress Intensity Factor K(Q) for AA2519–AA1050–Ti6Al4V Layered Material
title_sort analytic model of maximal experimental value of stress intensity factor k(q) for aa2519–aa1050–ti6al4v layered material
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7579026/
https://www.ncbi.nlm.nih.gov/pubmed/33036246
http://dx.doi.org/10.3390/ma13194439
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