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178 ALEKSANDR KORJAKIN ET AL.<br />
∂u<br />
∂γ x<br />
ε xx = + x3 =Ω xx + x3χxx<br />
∂x<br />
∂x<br />
1 ⎛ ∂v<br />
⎞ x ∂γ<br />
ε = + + =Ω + χ<br />
R⎝<br />
⎜<br />
∂ϕ ⎠<br />
⎟<br />
R ∂ϕ<br />
3 ϕ<br />
ϕϕ w<br />
ϕϕ x3<br />
ϕϕ<br />
1 ∂u<br />
∂v<br />
⎛ 1 ∂γ ∂γ ⎞<br />
γ = + + + = Ω + χ<br />
R ∂ϕ ∂x ⎜<br />
⎝R ∂ϕ ∂x<br />
⎟<br />
⎠<br />
x ϕ<br />
xϕ x3 2 xϕ 2x3<br />
xϕ<br />
∂w<br />
γ xx = γ 2<br />
3 x + = Ωxx<br />
3<br />
∂x<br />
1 ⎛∂w<br />
⎞<br />
γ = γ + − v = 2Ω<br />
R<br />
⎜<br />
⎝∂ϕ<br />
⎟<br />
⎠<br />
ϕx3 ϕ ϕx3<br />
(13)<br />
where R is the reference surface radius of the cylinder, ε xx , ε ϕϕ are the normal<br />
strains, and γ xϕ , γ xx , γ<br />
3 ϕx<br />
are the shear strains. In addition, Ω<br />
3<br />
xx , Ω ϕϕ , Ω xϕ denote<br />
the membrane strains, χ xx , χ ϕϕ , χ xϕ are the bending strains and Ω xx , Ω<br />
3 ϕx<br />
are the<br />
3<br />
transverse shear strains in the reference surface, respectively. The general<br />
strain-displacement relations for conical shells (see Figure 3) are given by<br />
∂u<br />
∂γ<br />
ε = + =Ω + χ<br />
∂x<br />
∂x<br />
x<br />
xx x3 xx x3<br />
xx<br />
1 ⎛ ∂v<br />
⎞<br />
ε ϕϕ = usin<br />
wcos<br />
r<br />
⎜ β+ + β<br />
⎝ ∂ϕ<br />
⎟<br />
⎠<br />
x3<br />
⎡ ∂γ ϕ cosβ⎛<br />
∂v<br />
⎞⎤<br />
+ ⎢γx<br />
sinβ+ + + usinβ+ wcosβ ⎥ =Ω ϕϕ + x3χ<br />
r<br />
∂ϕ r<br />
⎜<br />
⎝∂ϕ<br />
⎟<br />
⎣<br />
⎠⎦<br />
ϕϕ<br />
1 ∂u ∂v v<br />
γ xϕ<br />
= + − sinβ<br />
r ∂ϕ ∂x r<br />
⎛1∂γ<br />
∂γ<br />
x ϕ γ ϕ cosβ∂v⎞<br />
+ x3⎜<br />
+ − sinβ+ = 2Ω xϕ<br />
+ 2x3χ<br />
⎝r ∂ϕ ∂x r r ∂x<br />
⎟<br />
⎠<br />
xϕ<br />
(14)<br />
∂w<br />
= 2Ω<br />
x<br />
γ xx = γ<br />
3 x + xx ∂<br />
3<br />
1 ⎛∂w<br />
⎞<br />
γ = γ + − v cosβ = 2Ω<br />
r<br />
⎜<br />
⎝∂ϕ<br />
⎟<br />
⎠<br />
ϕx3 ϕ ϕx3<br />
where r = r(z) is the reference surface radius and β is the semi-vertex angle. The<br />
generalstrain-displacement relations for spherical shell (see Figure 4) are givenby