A structural plate component of an engineering design must support 207 MPa in tension. If aluminium alloy 2024-T851 is used for the application, calculate the the largest internal flaw size that this materials can support. given Y=1 ,K1c =26.4
A structural plate component of an engineering design must support 207 MPa in tension. If aluminium alloy 2024-T851 is used for the application, calculate the the largest internal flaw size that this materials can support. given Y=1 ,K1c =26.4
Materials Science And Engineering Properties
1st Edition
ISBN:9781111988609
Author:Charles Gilmore
Publisher:Charles Gilmore
Chapter6: Introduction To Mechanical Properties
Section: Chapter Questions
Problem 6.13P
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A structural plate component of an engineering design must support 207 MPa in tension. If aluminium alloy 2024-T851 is used for the application, calculate the the largest internal flaw size that this materials can support. given Y=1 ,K1c =26.4
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