from an aluminum alloy that has a plane strain fracture toughness of 45 MPa m and a yield strength of 500 MPa. It has been determined that fracture results at a stress of 250 MPa when the maximum internal crack length is 9 mm. For this same component and alloy, determine critical internal crack length that will result to fracture if the design stress is three-fourth of the yield strength. If the available flaw detection apparatus has a resolution limit of 3 mm, will the crack in (1) be detected? Why or why not? Show complete solution
from an aluminum alloy that has a plane strain fracture toughness of 45 MPa m and a yield strength of 500 MPa. It has been determined that fracture results at a stress of 250 MPa when the maximum internal crack length is 9 mm. For this same component and alloy, determine critical internal crack length that will result to fracture if the design stress is three-fourth of the yield strength. If the available flaw detection apparatus has a resolution limit of 3 mm, will the crack in (1) be detected? Why or why not? Show complete solution
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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An aircraft component is to be fabricated from an aluminum alloy that has a plane strain fracture toughness of 45 MPa m and a yield strength of 500 MPa. It has been determined that fracture results at a stress of 250 MPa when the maximum internal crack length is 9 mm.
- For this same component and alloy, determine critical internal crack length that will result to fracture if the design stress is three-fourth of the yield strength.
- If the available flaw detection apparatus has a resolution limit of 3 mm, will the crack in (1) be detected? Why or why not?
Show complete solution
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