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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)

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