Problem 11.17. Truncated cone with not adequate membrane support

Assume that the cone shown in the Figure is supported vertically only at the bottom. The truncated cone is subjected to a vertical line load, p = 10 kN/m at the upper edge. The radius of the top edge of the cone is a1 = 10 m, the radius of the bottom edge of the cone is a2 = 20 m, α0 = 60°. Thickness of the shell is h = 10 cm. Determine the bending moment.

Membrane solution of the cone is derived in Example 11.2.

Solve Problem

Solve

Maximum bending moment, Mmax [kNm/m]=

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Steps

Step by step

Follow steps in Example 11.11.

Step 1. Calculate the vertical reaction force.

Check vertical reaction

The vertical support force, A is calculated from the vertical equilibrium:

See Example 11.2.

A=p2a1π2a2π=pa1a2=10.010.020.0=5.00 kNm

Step 2. Determine the force component which causes the bending of the edge.

Check perpendicular component

A has a component in the direction of the meridian force and one which is perpendicular to it, the latter one, A – which is equal to the shear force at the edge – causes the bending of the shell.

A=Acosα=5.00×cos60°=2.50 kNm

Step 3. Calculate the bending moment from the edge disturbance.

Check moment

The moment is approximated by the moment of the osculating cylinder subjected to a line load, A:

See Figure 10.45a and Eq.(11-82).

Mmax=p2λ3D0.64λ2D=A0.32λ=A0.321.32Rh=A0.321.32a2sinαh=         =2.500.321.3220.0sin60°×0.1=0.9210 kNmm

The maximum bending moment occurs at a distance

0.6Rt=0.620.0sin60°×0.1=0.9118 m

from the bottom of the cone.

Results

Worked out solution

Follow steps in Example 11.11.

The vertical support force, A is calculated from the vertical equilibrium:

See Example 11.2.

A=p2a1π2a2π=pa1a2=10.010.020.0=5.00 kNm

A has a component in the direction of the meridian force and one which is perpendicular to it, the latter one, A – which is equal to the shear force at the edge – causes the bending of the shell.

A=Acosα=5.00×cos60°=2.50 kNm

The moment is approximated by the moment of the osculating cylinder subjected to a line load, A:

See Figure 10.45a and Eq.(11-82).

Mmax=p2λ3D0.64λ2D=A0.32λ=A0.321.32Rh=A0.321.32a2sinαh=         =2.500.321.3220.0sin60°×0.1=0.9210 kNmm

The maximum bending moment occurs at a distance

0.6Rt=0.620.0sin60°×0.1=0.9118 m

from the bottom of the cone.