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forces
bearing on them and how the internal forces are distributed within them.
That is, |
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they
exhibit plate action as opposed to the lattice action we just covered.
The equation |
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describing the stability of pure plate structures is: |
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. |
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E = 3 F - 6
where E = edges |
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F = faces |
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. |
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Notice
that, in terms of plate action, this equation asserts that the cube plate
structure just |
|
pictured
in Fig. 203 is stable. But the cube lattice structure is not
stable. Why is this so? |
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. |
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Pure
plate structures are entirely composed of rigid plates that are joined
together edge to |
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edge
with flexible hinge joints. These edges are called shear lines
because the internal |
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stresses
generated by an external load are distributed over the surface area of
the plates, |
|
which are
then concentrated as shear forces along the entire length of the edges
where the |
|
|
plates are joined. This shear force consists of a pair of
equal, |
|
 |
parallel forces acting in opposite directions with no distance |
|
between them, as shown in the animation to the left. Note |
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how pressing on the opposite vertices of the cube plate |
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structure causes the plates to shear past each other when |
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there is no hinge pin, or pinge, to resist this stress.
Normally |
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the pinges of the structure resist this shearing when they are |
|
positioned between the plates. The pinges, plus the rigidity
|
|
(demonstration model) |
of
the plates enables the structure to achieve a state of stable |
|
Fig. 204 - Plates of a cube |
equilibrium so that it resists shear failure when loaded. Due |
|
shearing past each other |
to
the hinge able nature of this joint the plates do not
|
| |
experience bending moments when the structure is loaded at |
|
|
its
vertices. Therefore pure plate structures are statically
determinate, although the static |
|
analysis
techniques are considerably more complex than those for trusses, or even
lattices. |
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. |
|
The
following images show building sections that are modeled as plate
structures. Each is |
|
 |
 |
 |
 |
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a) 9 = 3 ( 5 ) - 6 |
*b) 9 = 3 ( 5 ) - 6 |
*c) 12 = 3 ( 6 ) - 6 |
d) 8 < 3 ( 5 ) - 6 |
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stable |
stable |
stable |
unstable |
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click image to enlarge |
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Fig. 205 - Plate stability analysis of structures
(static demonstration models) |
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|
* Note:
for modeling purposes, all panels lying in the same plane are counted as
one plate |
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. |
|
analyzed
for its stability as a pure plate structure using E = 3 F - 6. Note
that most of the |
|
models
are stable except d), a square pyramid peaked roof. It is
undoubtedly rigid since |
|
. |
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Back
to Knowhere |
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Page 121
- Building stability - Plate action |
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