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Wood-Armer calculation (for plate elements)
It is reasonably common in bridge design that RC slabs must
be designed to resist a combination of moments (Mx, My) and a
twisting moment (Mxy) using orthogonal reinforcement.
In Concrete magazine (February 1968), R H Wood proposed a
procedure for "The Reinforcement of Slabs in Accordance
with a Pre-determined Field of Moments".
The following correspondence included additional
equations derived for skew slabs (principle moment directions
inclined to the reinforcement directions).
Together the equations are known as the Wood Armer equations.
For a full explanation and derivation of the formulae, the
reader is referred to either:
- "Concrete slabs: analysis and design" L.A Clark
and R.J Cope (Elsevier Applied Science)
- "Concrete Bridge Design to BS5400" L.A Clark
(Construction Press) Chapter 5 (section entitled
"Reinforced Concrete Plates") and Appendix A
By
reference to "Concrete Bridge Design to BS5400" Chapter
5 (section entitled "Reinforced Concrete Plates") and
Appendix A, the Wood-Armer calculation may be carried out by
following the procedure below.
All calculations proceed after the determination of the
moment field Mx, My, Mxy. The
equations have been amended to suit the sign convention for stress
results from LUSAS, and are described in a form that can be
translated directly to a spreadsheet format:
Top
(hogging) reinforcement
-
Determine
the generalized Wood-Armer moments:
MxT1=Mx+2*Mxy*cotø+My*(cotø)^2+ABS((Mxy+My*cotø)/sinø)
MøT1=My/((sinø)^2)+ABS((Mxy+My*cotø)/sinø)
-
Suppose
MxT1<0; section is in X-direction sagging
MxT2=0
MøT2=(1/(sinø)^2)*(My+ABS((Mxy+My*cotø)^2/(Mx+2*Mxy*cotø+My*(cotø)^2)))
-
Suppose
MøT1<0; section is in Y-direction sagging
MxT3=Mx+2*Mxy*cotø+My*(cotø)^2+ABS((Mxy+My*cotø)^2/My)
MøT3=0
-
Select
the appropriate values from the above for output.
Note that if MxT1<0 and MøT1<0,
then no top reinforcement is required
Mx(T)=IF(MøT1<0,IF(MxT3<0,0,MxT3),IF(MxT1<0,0,MxT1))
Mø(T)=IF(MxT1<0,IF(MøT2<0,0,MøT2),IF(MøT1<0,0,MøT1))
Bottom
(sagging) reinforcement
-
Determine
the generalized Wood-Armer moments:
MxB1=Mx+2*Mxy*cotø+My*(cotø)^2-ABS((Mxy+My*cotø)/sinø)
MøB1=My/((sinø)^2)-ABS((Mxy+My*cotø)/sinø)
-
Suppose
MxB1>0; section is in X-direction hogging
MxB2=0
MøB2
=(1/(sinø)^2)*(My-ABS((Mxy+My*cotø)^2/(Mx+2*Mxy*cotø+My*(cotø)^2)))
-
Suppose
MøB1>0; section is in Y-direction hogging
MxB3=Mx+2*Mxy*cotø+My*(cotø)^2-ABS((Mxy+My*cotø)^2/My)
MøT3=0
-
Select
the appropriate values from the above for output.
Note that if MxB1<0 and MøB1<0,
then no bottom reinforcement is required
Mx(B)=IF(MøB1>0,IF(MxB3>0,0,MxB3),IF(MxB1>0,0,MxB1))
Mø(B)=IF(MxB1>0,IF(MøB2>0,0,MøB2),IF(MøB1>0,0,MøB1))
A simple example may be used to
demonstrate the Wood Armer calculation for orthogonally placed (minimised area) reinforcement.
A simply supported rectangular slab in subjected to a
uniform pressure: no in-plane forces (Nx, Ny, Nxy) will be
generated and a cursory check of the primary results ahead of
the Wood Armer calculations is possible.
The example will generate a generally sagging field of
moments, however by reversal of the load, all the Wood Armer calculations for orthogonally placed
(minimised area)
reinforcement carried out by LUSAS may be checked if necessary.
- Rectangular
surface, plan dimensions length 16 units, width 10 units
- Mesh attributes: Any quadrilateral plate or shell element
(QSI4 elements used in subsequent calcs) regular mesh of element size 1 unit
- Geometric attributes: thickness 0.2 units
- Material attributes: E=1E6, poisson's ratio=0.3
- Supports: pinned on all 4 sides viz.
- Left & right = fixed in translation
(X,Y,Z) fixed in
rotation (X only)
- Top & bottom = fixed in translation
(X,Y,Z) fixed in
rotation (Y only)
- Loading attributes: Structural load, global distributed Z
direction 1.0unit/unit area
Download
Wood Armer example model (LUSAS mdl file)
Cursory Check on primary results
|
Theoretical
|
LUSAS
Results
|
|
Deflection at
centre node
|
-0.1134
|
-0.1122
|
|
Mx (max) at
centre node
|
-8.62
|
-8.62
|
|
My (max) at
centre node
|
-4.92
|
-4.93
|
Moment field from LUSAS Modeller, extracted at 4 nodes for
calculations to be checked explicitly:
|
Node
|
61
|
111
|
124
|
162
|
|
Mx
|
-0.996
|
-8.504
|
-3.300
|
-3.771
|
|
My
|
-0.833
|
-4.913
|
-1.715
|
-2.614
|
|
Mxy
|
-3.847
|
-2.26E-14
|
1.26E-14
|
-2.378
|
Calculation of Wood Armer moments by hand, determined from
the moment field (Mx, My, Mxy) using the procedure explained
above. Download
spreadsheet calculations (MSExcel format)
|
Node
|
61
|
111
|
124
|
162
|
|
Mx(T)
|
2.852
|
0.000
|
0.000
|
0.000
|
|
My(T)
|
3.014
|
0.000
|
0.000
|
0.000
|
|
Mx(B)
|
-4.843
|
-8.504
|
-3.300
|
-6.149
|
|
My(B)
|
-4.680
|
-4.913
|
-1.715
|
-4.992
|
Wood Armer Moments from LUSAS
Modeller, extracted at the same
4 nodes for comparison to the hand calculations undertaken:
|
Node
|
61
|
111
|
124
|
162
|
|
Mx(T)
|
2.852
|
0.000
|
0.000
|
0.000
|
|
My(T)
|
3.014
|
0.000
|
0.000
|
0.000
|
|
Mx(B)
|
-4.842
|
-8.504
|
-3.300
|
-6.149
|
|
My(B)
|
-4.680
|
-4.913
|
-1.715
|
-4.992
|
By inspection the results tabulated above agree
closely with those derived by hand calculation and demonstrate that
the Wood Armer calculations for this example are satisfactory.
Other Wood Armer
related topics
|