6. Design for , that is, the load can be taken by other members or the effect of fatigue failure otherwise mitigated, until the failed component can be detected and repaired or replaced. This approach is common in aircraft structural design. 7. create variations in dimensions, which can affect wear and fatigue properties. 8. is often used as the starting point to identify the most important problems and the most likel causes. blish

6. Design for , that is, the load can be taken by other members or the effect of fatigue failure otherwise mitigated, until the failed component can be detected and repaired or replaced. This approach is common in aircraft structural design. 7. create variations in dimensions, which can affect wear and fatigue properties. 8. is often used as the starting point to identify the most important problems and the most likel causes. blish

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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