کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
1576312 | 1514775 | 2013 | 7 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Microstructure-fracture toughness correlation in an aircraft structural component alloy Ti-5Al-5V-5Mo-3Cr
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
مهندسی مواد
دانش مواد (عمومی)
پیش نمایش صفحه اول مقاله
![عکس صفحه اول مقاله: Microstructure-fracture toughness correlation in an aircraft structural component alloy Ti-5Al-5V-5Mo-3Cr Microstructure-fracture toughness correlation in an aircraft structural component alloy Ti-5Al-5V-5Mo-3Cr](/preview/png/1576312.png)
چکیده انگلیسی
Ti-5Al-5V-5Mo-3Cr alloy is a relatively new alloy developed for aircraft structural application where fracture toughness is an important property of consideration. A systematic variation of processing parameters has been carried out to generate different beta annealed microstructures, in terms of their dimensions in this alloy. Quantitative measurements of microstructural features have been carried out using stereological procedures. Different length scales of features have been correlated with the fracture toughness in order to optimize the processing parameters to develop desired microstructure that results in improved fracture toughness. The change in fracture mode associated with different microstructures has been investigated using fractographic analysis.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Materials Science and Engineering: A - Volume 568, 15 April 2013, Pages 61-67
Journal: Materials Science and Engineering: A - Volume 568, 15 April 2013, Pages 61-67
نویسندگان
Atasi Ghosh, S. Sivaprasad, Amit Bhattacharjee, Sujoy Kumar Kar,