d.N A fatigue crack growth test is being carried out on a large steel plate containing a 2 mm edge crack. The growth of cracks can be well represented by the Paris Law da= A(AK)*, where A is a constant (4= 6.6 × 10-¹³ (MPa) m cycle") and 4K = Kmax-Kin. If the plate is subjected to a fatigue stress for which max 120 MPa and a ratio R = -0.25 (R=Gmin/max) at a frequency of 2 Hz (2 cycles per second), how long will the crack grow to after 10 hours? and K for the edge crack is K = 1.12 o√(na) Note that: da 1 1 (4-4-4 —— a, (A) 2.6 mm (B) 3 mm (C) 7.2 mm (D) 8 mm (E) 10 mm
d.N A fatigue crack growth test is being carried out on a large steel plate containing a 2 mm edge crack. The growth of cracks can be well represented by the Paris Law da= A(AK)*, where A is a constant (4= 6.6 × 10-¹³ (MPa) m cycle") and 4K = Kmax-Kin. If the plate is subjected to a fatigue stress for which max 120 MPa and a ratio R = -0.25 (R=Gmin/max) at a frequency of 2 Hz (2 cycles per second), how long will the crack grow to after 10 hours? and K for the edge crack is K = 1.12 o√(na) Note that: da 1 1 (4-4-4 —— a, (A) 2.6 mm (B) 3 mm (C) 7.2 mm (D) 8 mm (E) 10 mm
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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Transcribed Image Text:TS8
dN
A fatigue crack growth test is being carried out on a large steel plate containing a 2 mm edge
crack. The growth of cracks can be well represented by the Paris Law da = A(AK)*, where A
is a constant (4= 6.6 × 10-¹³ (MPa) m cycle") and 4K = Kmax-Kin. If the plate is subjected
to a fatigue stress for which max 120 MPa and a ratio R = -0.25 (R=0min/max) at a frequency
of 2 Hz (2 cycles per second), how long will the crack grow to after 10 hours?
Note that:
Sorda - 12-
=
a²
(A) 2.6 mm
(B) 3 mm
(C) 7.2 mm
(D)
8 mm
(E) 10 mm
a
and K for the edge crack is K= 1.12 o√(na)
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