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124 CHAPTER 5. TORSION<br />

Q 1<br />

i 3<br />

R<br />

i 2<br />

i 3<br />

Circular<br />

cylinder<br />

i 2<br />

R i<br />

R o<br />

i 3<br />

Circular<br />

annulus<br />

Figure 5.1: Circular cylinder with end torques.<br />

written as the projection of this displacement along directions ī2 and ī3, respectively,<br />

u2(x1, r, α) = −rφ1(x1) sin α; u3(x1, r, α) = rφ1(x1) cos α. (5.1)<br />

Since the cross-section does not deform out of its own plane, the axial displacement field must vanish,<br />

i.e. u1(x1, x2, x3) = 0. Finally, the transformation from polar to Cartesian coordinates is<br />

i 1<br />

i 2<br />

Q1<br />

x2 = r cos α; x3 = r sin α. (5.2)<br />

The complete displacement field describing the torsion of circular cylinders expressed in Cartesian coordinates<br />

can now be written by substituting eq. (5.2) in (5.1) to yield<br />

and<br />

u2(x1, x2, x3) = −x3φ1(x1); u3(x1, x2, x3) = x2φ1(x1) (5.3)<br />

u1(x1, x2, x3) = 0. (5.4)<br />

The corresponding strain field is readily obtained using the strain-displacement equations as:<br />

ε1 = ∂u1<br />

= 0; (5.5)<br />

∂x1<br />

ε2 = ∂u2<br />

= 0; ε3 =<br />

∂x2<br />

∂u3<br />

= 0; γ23 =<br />

∂x3<br />

∂u2<br />

+<br />

∂x3<br />

∂u3<br />

= 0; (5.6)<br />

∂x2<br />

γ12 = ∂u1<br />

+<br />

∂x2<br />

∂u2<br />

∂x1<br />

= −x3 κ1(x1); γ13 = ∂u1<br />

+<br />

∂x3<br />

∂u3<br />

∂x1<br />

= x2 κ1(x1), (5.7)<br />

where the sectional twist rate is defined as<br />

κ1(x1) = dφ1<br />

. (5.8)<br />

dx1<br />

The section twist rate, κ1, measures the deformation of the circular cylinder. The twist angle, φ1, simply<br />

measures the rotation of any section with respect to a reference. Note that a constant twist angle implies a<br />

rigid body rotation of the cylinder about its axis, but no deformation.

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