2000
WESDEF
OCA
ILLIBACK
WESDEF
CWA
1600
ILLIBACK
y = 0.0003 ISM 2 0.0365 ISM + 72.57
2
R = 0.73
1200
y = 0.0004 ISM 2 + 0.1378 ISM + 41.57
R2 = 0.96
800
400
Figure 27. Relationship between ISM and
0
400
800
1200
1600
2000
subgrade modulus at OCA and CWA.
ISM (MN/m)
best fit the data, so for estimation, a single power
In Figure 27, the relationship of ISM and subgrade
trend was applied to the data as shown in Figure 25c.
modulus for both OCA and CWA is shown. Again, a
Figure 26 shows the relationship between the meas-
single power curve can be fitted to the data.
ured total basin area and the coefficient of subgrade
Current criteria for PCC pavements state that failure
reaction (k) computed from ILLIBACK for both sites
occurs when the horizontal tensile stress at the bottom
The following equations have been developed from
of the PCC layer is equal to or greater than the flexural
the ILLIBACK results and can be used to estimate the
strength of the slab. The flexural strength reported at
subgrade modulus and the coefficient of subgrade re-
OCA and CWA was 4.5 MPa. The two types of aircraft
action (k)
used for these simulations were the MD-DC9 and the
Boeing 757. The gear loads, tire spacings and radii
SM = 240,185AT1.248
(R2 = 0.91)
were obtained from the FAALEA computer program
and are presented in Tables 8 and 9.
k = 741, 480 AT1.6662
(R2 = 0.86)
Several FWD locations were selected from each air-
port for computing the tensile stress at the bottom of the
where SM = subgrade modulus (MPa)
PCC layer on different days during the monitoring peri-
AT = total basin area (mm2)
od. The damage (D) reported here is defined as the ratio
k = coefficient of subgrade reaction
of maximum horizontal (tensile) stress to the flexural
(MN/m3).
Table 8. Gear loading for the MD-DC9 and Boeing 757.
Aircraft
Design load % of design load Load on main gear
type
(MN)
on each main gear
(MN)
MD-DC9
480
47.5
228.2
Boeing 757
1112
47.5
528.2
Table 9. Gear information for computer simulations of the
MD-DC9 and Boeing 757.
Contact Contact Load on
Aircraft
Tire Radius
area
pressure
tire
X-cord
Y-cord
2)
type
no. (mm)
(m
(kPa)
(kN)
(mm)
(mm)
MD-DC9
1
181.4
0.103
1103
114.1
330.2
0
2
181.4
0.103
1103
114.1
330.2
0
Boeing 757 1
189.5
0.113
1172
132.1
431.8
0
2
189.5
0.113
1172
132.1
431.8
0
3
189.5
0.113
1172
132.1
431.8
1143
4
189.5
0.113
1172
132.1
431.8
1143
24