6- STRAINS COMPUTATION
The strains are calculated from the values
of the vertical and horizontal
displacement at the nodes of the grid.
Each element of the grid is considered to
be a square element (12.5mm X 12.5mm).
The vertical and horizontal strains are
calculated through the centre of the
element. The following assumptions
(James, 1972) apply:
1- displacements vary linearly across each
element which in turn assumes that the
sand in every element strains uniformely.
2- changes in the geometry of the system
during testing have a negligible effect on
the caleulated strains.
3- compressive strains are assumed to be
positive.
The shear strain is defined as the angular
distortion at the centre of the element
taken from the top right hand quarter of
the element and is calculated from the
appropriate vertical and horizontal
displacements of the four corners of the
element. All the strain values are
assigned to the centres of the elements
and the coordinates of the nodes of the
grid containing the strains are redefined
to these positions. The nodal points of
each element are numbered proceeding in a
counterclockwise direction around the
element in the order 1,2,3 and 4 (fig. 2).
y Va Vv
T
u42 > u
4 3 3
- WwW
Fig.2 Numbering convention for
the nodal points.
The following equations were derived :
e UE (u, ;4.u,) - (Cu, v u)
x 2x
. (v tV = (Va i Va)
y 2y
Yxy7 [((v;-v9)*(v,-v,))72x] *
FCCuzzu, 90 (u,7u,))72y]
Where, ‘x , ‘> and Y:;y are the axial strains
and shear strain respectively. u and wv
represent the horizontal and vertical
displacement.
7- TESTING PROCEDURE
The apparatus consisted of a wooden box,
600 om by 300 cm in plan and 400 cm depth.
The front viewing face of the box was
designated to allow a 6 mm thick glass to
slide in and out. Sufficiently stiff
bracing for this glass face was obtained
on the bottom and sides of the tank by the
use of thin U metal plates. It was
restrained against the frame by bolts
screwed through tapped holes in the front
of the box.
with 5 mm inside diameter was fixed in the
base at the centre of the box immediately
behind the glass face. À semi circular
brass disc 50 mm diameter and 13 mm thick
was welded to the upper end of 5 mm
diameter shaft to make the anchor unit.
The shaft was 400 mm long, its diameter
having been reduced to 5 mm from the
middle to the upper end in order to be
pushed through the bush. The bottom end
of the shaft was fixed to a load cell
which in turn was fixed to the base plate
of a 1 ton Whykeham Farrance multispeed
machine. À Sangamo transducer was
also fixed to the base plate to record the
displacement of the plate anchor. The
load cell and the LVDT were connected to a
data logger and a plotter in order to
monitor the different stages of the test.
The sand was placed in layers of 30 mm
thickness until the required depth was
reached , a rectangular hopper, 650 mm by
300 mm in plan and 300 mm in depth, being
used to produce a rain of sand grains and
therefore achieve the required densities.
Details of the technique have already been
given in Bouazza (1990) and Bouazza &
Finlay (1990).
120
I00 r
Push out load P (N)
1 1 J 1 —
0 I 2 3 4 5 6
Displacement ¢ (mm)
FIG.3: TYPICAL LOAD VS DISPLACEMENT CURVE.
A semi circular brass bush.