Fatigue Crack Paths 2003
SIFs F O RC Y L I N D R I CAANLDS P H E R I CSAHLE L L S
Cylindrical Shell underInternal Pressure
The actual hoop stress distribution, 610,10”), in an unnotched cylinder (R1 = 00, R2 = 25
m m , r = <><>) under an internal pressure p can be written as follows [1 l]:
_ p (R. —02 “WM-R;-(R.-t>2i
R5
6 (i
“i
For a longitudinal surface flaw, an approximate expression of the dimensionless SIF,
K >kl(p,cu) ’
along the crack front can be determined through the superposition principle
(see Eq.4, [8]) :
1
5
Z Bn(p,cu) K*I(n)
(7)
K
i
*
:
101.611)
%fmcu)H20
where o'reflp’cu) = p R /t is the well-known uniform hoop stress in a thin-walled pipe
under internal pressure (R = meanradius of the cylinder), and the coefficients Bnumu)
(see Eq. 5) are listed in Table 1.
Table 1. Coefficients of series expansion for a cylindrical shell under an internal pressure.
(R2 —02
R2
r (R —02
R2
"P’ > W 1e —(a —02 (R. +w-ar
“W” R; —0. —02 (R. —a)2 i
Bl
: _ 2 P(R2 ‘02 _
R22
_a
B2 = 3P (R2 _t)2 _
R22
_a2
(PM)
R2 —(R2 _I)2 (R, _..)3
W") R; —(R. —02 (R. —a)“
B I L i i w g B = M R? _a4 _
3 (My)
R22 _(R2 ‘02 (R2 _a)5
4 (Wu)
R22 _(R2 _t)2 (R2 _a)6
B ( )_ _6P(R2_t)2_ R22
_a5
5 p,cu _ R 2 _ ( _Rt)2 (R _ a ) 7 2 2 2
In the case of a notched cylindrical shell, the analytical solution for the hoop stress
distribution 610,96) (w) is not available. Therefore, o'1(p’c)(w) must numerically be
computed in order to obtain the coefficients Bnmc). The reference stress can
conveniently be defined as o'ref(p,c) : pR/t', and the dimensionless SIF, K *up’c), can
be obtained from an expression similar to Eq. 7, where the subscript cu is replaced by c.
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