PSI - Issue 52
A.D. Cummings et al. / Procedia Structural Integrity 52 (2024) 762–784 A. Cummings / Structural Integrity Procedia 00 (2023) 000–000
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Table 2. Mechanical and impact properties of package body BS1503 224 430 LT40 Property Room Temperature ( ≈ 23 ◦ C)
Low Temperature (-40 ◦ C)
E [MPa]
205,000
209,000*
0.3
0.3
ν
3 ]
7,900
7,900 340* 509*
ρ [kg / m
σ y [MPa] σ uts [MPa]
290 466 0.34 N / A N / A
N / A
elong
Charpy [J] (A) Charpy [J] (B)
52 91
K mat is calculated from the master curve equation, Eqn J.5 BS7910 (2019):- K mat = 20 + { 11 + 77 exp [0 . 019( T − T 0 − T K )] } 25 B 0 . 25 ln 1 1 − p f 0 . 25 WhereT 0 is found from the following three equations:- Eqn J.6 BS7910 (2019):- T 27 J = T Cv − C 4 ln C v ( C us v − 27) 27( C us v − C v )
(1)
(2)
C is calculated from Eqn J.7 BS7910 (2019):-
C us v 14 . 3
σ y − 40 ◦ C
C = 34 ◦ C +
(3)
35 . 1 −
And Eqn J.4 BS7910 (2019) provides:-
1000 C us v
σ YRT 12
T 0 = T 27 J − 87 +
(4)
+
T 0 is then corrected to account for dynamic e ff ects by applying Eqn L.15 BS7910 (2019):-
T 0 , st ln ( ˙ K ) Γ − ln ( ˙ K )
(5)
∆ T 0 =
Where Γ is found from Eqn L.16 BS7910 (2019):- Γ= 9 . 9 exp T 0 , st 190 1 . 66 + σ y 722 1 . 09
(6)
Where σ y is the yield stress at the T 0 , st temperature (estimated using equations in chapter 7 BS7910 (2019)) and ˙ K is estimated as Meyers (1994):-
K mat t f
˙ K =
(7)
The final value depends on the thickness of the member at the stressed location and the time to fracture, t f . In the centre of the package base and internal radius, which are highly stressed in a base down drop (as will be shown), K mat = 34MPa.m 0 . 5 andK mat = 33.6MPa.m 0 . 5 respectively. The master curve approach, originally developed for ferritic steels, has been validated for a similar grade of ma terial, ASTM A350 LF5 Norton et al. (2004). It is therefore expected that the fracture toughness estimates are conservative.
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