Problem 2: A catastrophic failure occurred to a 7079-T6 aluminum alloy shaft. The maximum tensile stress was specified as 30% of the yield stress (oy = 300 MPa) and the stress ratio R was zero. Post-failure examination found that fatigue crack growth striation started at a depth of 2.0 cm from the surface, and the striation spacing was 1.3 x 10-4 cm. The fatigue-crack growth behavior of the aluminum alloy is given in the right figure. The manufacturer claimed that the part was overloaded by the user, but the user denied the allegation and sued the manufacturer. As a mechanical engineer, what is your verdict based on your calculation?

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Problem 2: A catastrophic failure occurred to a 7079-T6
aluminum alloy shaft. The maximum tensile stress was
specified as 30% of the yield stress (0₂ = 300 MPa) and
the stress ratio R was zero. Post-failure examination
found that fatigue crack growth striation started at a
depth of 2.0 cm from the surface, and the striation
spacing was 1.3 x 10-4 cm. The fatigue-crack growth
behavior of the aluminum alloy is given in the right
figure. The manufacturer claimed that the part was
overloaded by the user, but the user denied the
allegation and sued the manufacturer. As a mechanical
engineer, what is your verdict based on your
calculation?
da/dN (μm)/cycle
4 6 8 10
2.5TTTTT
1.0
0.25
Titanium
Aluminum
0.05-
10
20
30
ksi Vin
40 60 80 100
• 200 Som
200
T
-Steel
80
AK (MN/m2)
400 600 1000
•
A533 alloy steel
Ni-Mo-V alloy steel
A HP 9-4-25 alloy steel
7079-T6 aluminum alloy
5456-H321 aluminum alloy
Ti-6 Al-4V titanium alloy
L
180
T
600
100
480
460
40
uin./cycle
Transcribed Image Text:Problem 2: A catastrophic failure occurred to a 7079-T6 aluminum alloy shaft. The maximum tensile stress was specified as 30% of the yield stress (0₂ = 300 MPa) and the stress ratio R was zero. Post-failure examination found that fatigue crack growth striation started at a depth of 2.0 cm from the surface, and the striation spacing was 1.3 x 10-4 cm. The fatigue-crack growth behavior of the aluminum alloy is given in the right figure. The manufacturer claimed that the part was overloaded by the user, but the user denied the allegation and sued the manufacturer. As a mechanical engineer, what is your verdict based on your calculation? da/dN (μm)/cycle 4 6 8 10 2.5TTTTT 1.0 0.25 Titanium Aluminum 0.05- 10 20 30 ksi Vin 40 60 80 100 • 200 Som 200 T -Steel 80 AK (MN/m2) 400 600 1000 • A533 alloy steel Ni-Mo-V alloy steel A HP 9-4-25 alloy steel 7079-T6 aluminum alloy 5456-H321 aluminum alloy Ti-6 Al-4V titanium alloy L 180 T 600 100 480 460 40 uin./cycle
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