A hypothetical metal having a grain diameter of 0.0082 mm is heated to 500C for 12.5 min, the grain diameter increases to 0.027 mm. Compute the grain diameter when a specimen of the original material is heated at 500C for 100 min. Assume the grain diameter exponent n has a value of 2.
A hypothetical metal having a grain diameter of 0.0082 mm is heated to 500C for 12.5 min, the grain diameter increases to 0.027 mm. Compute the grain diameter when a specimen of the original material is heated at 500C for 100 min. Assume the grain diameter exponent n has a value of 2.
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Problem
MUEGYETEM 1 7 8 2
A hypothetical metal having a grain diameter of 0.0082 mm is heated
to 500C for 12.5 min, the grain diameter increases to 0.027 mm.
Compute the grain diameter when a specimen of the original material
is heated at 500C for 100 min. Assume the grain diameter exponent n
has a value of 2.
10
62°F
ENG
10:30 PM
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5/10/2022](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F27650db4-f5f1-4bc5-af14-df805f1811e9%2F6d7cc84f-24eb-4045-8d2b-0250eb8572f2%2Fxkv7xs_processed.png&w=3840&q=75)
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Problem
MUEGYETEM 1 7 8 2
A hypothetical metal having a grain diameter of 0.0082 mm is heated
to 500C for 12.5 min, the grain diameter increases to 0.027 mm.
Compute the grain diameter when a specimen of the original material
is heated at 500C for 100 min. Assume the grain diameter exponent n
has a value of 2.
10
62°F
ENG
10:30 PM
qb
Clear
US
5/10/2022
![Po 22Mat_Eng_Test_16_fatigue_27_0 ×
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P 22_Mat_Eng_Test_17_creep_02_0 ×
Po 22_Mat_Eng_Test_17_creep_04_0 X
pDE 22_Mat_Eng_Test_17_creep_02_0 X
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Rupture lifetime
MÚE GYETEM 17 8 2
tf = A'o¬me(RT
1000
800
600
650°C
tf: time-to-failure/rupture lifetime
A', m, Qf: creep-failure constant
R= 8.31 J/mol·K
T: absolute temperature
400
730°C
200
925°C
815°C
100
80
60
40
What is the rupture lifetime for an S-590
alloy that is exposed to 400 MPa tensile
stress at 815 °C?
20
10-4
10-3
10-2
10-1
1 10
102
103
104
105
Rupture lifetime (h)
S-590 alloy (Fe, Cr, Ni, Co, W, Mo, Mn, C)
12
62°F
ENG
10:32 PM
qb
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US
5/10/2022
Stress (MPa)](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F27650db4-f5f1-4bc5-af14-df805f1811e9%2F6d7cc84f-24eb-4045-8d2b-0250eb8572f2%2F040wij_processed.png&w=3840&q=75)
Transcribed Image Text:Po 22Mat_Eng_Test_16_fatigue_27_0 ×
Po 22_Mat_Eng_Test_11_recryst_03_ X
P 22_Mat_Eng_Test_17_creep_02_0 ×
Po 22_Mat_Eng_Test_17_creep_04_0 X
pDE 22_Mat_Eng_Test_17_creep_02_0 X
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D Page view
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03
11
att
Rupture lifetime
MÚE GYETEM 17 8 2
tf = A'o¬me(RT
1000
800
600
650°C
tf: time-to-failure/rupture lifetime
A', m, Qf: creep-failure constant
R= 8.31 J/mol·K
T: absolute temperature
400
730°C
200
925°C
815°C
100
80
60
40
What is the rupture lifetime for an S-590
alloy that is exposed to 400 MPa tensile
stress at 815 °C?
20
10-4
10-3
10-2
10-1
1 10
102
103
104
105
Rupture lifetime (h)
S-590 alloy (Fe, Cr, Ni, Co, W, Mo, Mn, C)
12
62°F
ENG
10:32 PM
qb
Clear
US
5/10/2022
Stress (MPa)
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