Holooly Plus Logo

Question 15.4: The creep–rupture data for alloy S-590 plotted in Fig. 15.8 ...

The creep–rupture data for alloy S-590 plotted in Fig. 15.8 are given in Table E15.4(a), where, for each test, the temperature T, stress σ, and rupture time t_{r} are listed. Employ these data as follows:

(a) On the basis of Eq. 15.19,

\begin{gathered}\log t_r=P_{S D}+\frac{0.217 Q}{T} \quad \quad       (a) \\ P_{S D}=a_0+a_1 x+a_2 x^2+a_3 x^3 \quad \quad (b)\end{gathered}              (15.19)

obtain a fitted equation relating the Sherby–Dorn parameter to stress. Consider Q = 85,000 cal/mole from Table 15.2 to be given.

(b) Similarly, use Eq. 15.20

\begin{gathered}\log t_r=\frac{P_{L M}}{T}-C \quad \quad     (a) \\ P_{L M}=b_0+b_1 x+b_2 x^2+b_3 x^3 \quad \quad (b)\end{gathered}          (15.20)

to obtain a fitted equation relating the Larson–Miller parameter to stress, with C = 17 log (h) from Table 15.3 given.

Table E15.4(a)
T
K
σ

MPa

t_{r}

hours

T

K

σ

MPa

t_{r}

hours

T

K

σ

MPa

t_{r}

hours

811 690 22 922 345 93 1005 121 16 964
811 621 109 922 310 192 1089 172 25
811 552 433 922 276 756 1089 155 88
811 483 1677 922 241 2 243 1089 138 267
866 552 25 922 207 11 937 1089 121 719
866 517 44 922 172 43 978 1089 103 1 354
866 483 109 1005 234 59 1089 86 5 052
866 414 264 1005 193 342 1089 69 15 335
866 345 3149 1005 172 809 1089 69 11 257
922 414 26 1005 172 1028
922 379 63 1005 138 9 529
Source: Data in [Goldhoff 59a].

 

Table 15.2 Activation Energies for the Sherby–Dorn Parameter
Material 1Cr-1Mo-0.25V
steel
A-286
Fe-Ni-Cr alloy
S-590
Fe-Cr-Ni-Co alloy
Nimonic 80A
Ni-base alloy
Q, cal/mole 110,000 91,000 85,000 91,000
Source: Data in [Conway 69], [Goldhoff 59a], and [Goldhoff 59b].

 

Table 15.3 Constants for the Larson–Miller Parameter
C Polynomial Fit (units of hours, K, and MPa) Range of L-M Fit
Material log (hours) b_{0} b_{1} b_{2} b_{3} σ, Mpa T, K
1Cr-1Mo-0.25V steel 22 128,200 −141,500 64,380 −9,960 69–621 755–1005
AISI 310 stainless steel 10 20,470 -4,655 0 0 3.4–31 1255–1366
A-286 (Fe-Ni-Cr alloy) 20 116,400 −120,500 53,460 -8,188 69–758 811–1089
S-590 (Fe-Cr-Ni-Co alloy) 17 38,405 −8,206 0 0 69–690 811–1089
Nimonic 80A (Ni-base alloy) 18 16,510 11,040 −4,856 403 54–486 923–1089
Source: Values and data in [Conway 69], [Goldhoff 59a], [Goldhoff 59b], [Larson 52], [Orr 54], and [van Echo 67].
15.8
The "Step-by-Step Explanation" refers to a detailed and sequential breakdown of the solution or reasoning behind the answer. This comprehensive explanation walks through each step of the answer, offering you clarity and understanding.
Our explanations are based on the best information we have, but they may not always be right or fit every situation.
The blue check mark means that this solution has been answered and checked by an expert. This guarantees that the final answer is accurate.
Learn more on how we answer questions.
Already have an account?

Related Answered Questions

Question: 15.3

Verified Answer:

The logic is the same as before, except that now [...