Consider a wide, flat panel in an aircraft application which experiences fatigue stresses. The maximum stress is (150 Mpa) and the minimum stress in a cycle is zero. During inspection, (2 mm) deep flow has been found on the edge of the panel. Estimate the remaining fatigue life of the panel given the following material data. ksc = 30 Mpa vm da (2.5 x 10-12) (Ak)2.5 dN

Consider a wide, flat panel in an aircraft application which experiences fatigue stresses. The maximum stress is (150 Mpa) and the minimum stress in a cycle is zero. During inspection, (2 mm) deep flow has been found on the edge of the panel. Estimate the remaining fatigue life of the panel given the following material data. ksc = 30 Mpa vm da (2.5 x 10-12) (Ak)2.5 dN

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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