AIRY STRESS FUNCTION FOR TWO DIMENSIONAL INCLUSION ...
AIRY STRESS FUNCTION FOR TWO DIMENSIONAL INCLUSION ...
AIRY STRESS FUNCTION FOR TWO DIMENSIONAL INCLUSION ...
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Sz<br />
b b<br />
χ ( z)<br />
= (log z) b .<br />
z z<br />
−<br />
2<br />
2 3<br />
+ 1 − − 2<br />
4 2<br />
A plate with a hole is better manipulated using the polar coordinates.<br />
21<br />
(3.2.2)<br />
Substituting z re iθ<br />
= in (3.2.1) and (3.2.2) gives the Airy stress function in terms<br />
of the polar coordinates as<br />
1 4 2<br />
φ ( r,<br />
θ) = 2 ( Sr sin θ − b3 cos2θ + b1r log r<br />
2r<br />
2 2<br />
− 2b cosθ + 2a r cos2θ + 2a cos3θ + 2a cos 4θ).<br />
2 1 2 3<br />
(3.2.3)<br />
Applying (2.1.7) to the above Airy stress function, we get the stresses in polar<br />
form as follows:<br />
1 4 4<br />
2<br />
σ rr = 4 ( Sr + Sr cos2θ + 2b1r + 4b2r<br />
cosθ<br />
2r<br />
2<br />
+ 6b cos2θ − 8a r cos2θ − 20a r cos 3θ<br />
),<br />
3 1<br />
1 4 4<br />
2<br />
σ θθ = 4 ( Sr − Sr cos2θ − 2b1r − 4b2r<br />
cosθ<br />
2r<br />
− 6b cos2θ + 4a r cos 3θ<br />
),<br />
3 2<br />
1 4<br />
τ rθ<br />
= 4 ( − Sr sin 2θ + 4b2r sin θ + 6b3 sin2θ<br />
2r<br />
2<br />
− 4a r sin 2θ − 12a r sin 3θ<br />
).<br />
1<br />
The displacements can be determined using (2.2.11) as<br />
u<br />
r<br />
1<br />
4<br />
4 4<br />
= 3 ( − Sr + Sκ 1r<br />
− 2Sr cos2θ<br />
− 4b1r<br />
8µ<br />
r<br />
1<br />
2<br />
− 4b r cosθ − 4b cos2θ + 4a r cos2θ<br />
2 3 1<br />
2<br />
+ 4κ a r cos2θ + 8a r cos3θ + 4κ a r cos 3θ<br />
),<br />
1 1<br />
2<br />
2 1 2<br />
2<br />
2<br />
(3.2.4)<br />
(3.2.5)<br />
(3.2.6)<br />
(3.2.7)