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12.6 Flexible-Pavement <strong>Design</strong> Methods (U.S. Practice) 523<br />

where<br />

t = design thickness (in.)<br />

P = single-wheel load (lb)<br />

A = measured tire contact area (in. 2 )<br />

In 1959, the equation was modified to account for load repetitions <strong>and</strong> multiplewheel<br />

configurations. The modified equation employed the concept <strong>of</strong> an equivalent<br />

single-wheel load (ESWL):<br />

<br />

1/2 ESWL<br />

t = f<br />

(12.12)<br />

8.1(CBR) − A/π<br />

Section ACAggrega~01 in Job FAARFIELDPCRIGID01<br />

Working directory is C:\Program Files\FAA\FAARFIELD<br />

The structure is New Flexible. Asphalt CDF was not computed.<br />

<strong>Design</strong> Life = 20 Years<br />

A design for this section was completed on 02/23/10 at 19:55:37.<br />

Pavement Structure Information by Layer, Top First<br />

No.<br />

Type<br />

Thickness,<br />

in.<br />

Modulus,<br />

psi<br />

Poisson's<br />

Ratio<br />

Strength<br />

R.psi<br />

1<br />

P-401/P-403 HMA Surface 4.00 200,000 0.35 0<br />

2 P-401/P-403 St (flex) 11.00 400,000 0.35 0<br />

3 P-208 Cr Ag 19.88 57,845 0.35 0<br />

4 Subgrade 0.00 12,000 0.35 0<br />

Total thickness to the top <strong>of</strong> the subgrade = 35.88 in<br />

Airplane Information<br />

No.<br />

Name<br />

Gross Wt,<br />

Ib<br />

Annual<br />

Departures<br />

% Annual<br />

Growth<br />

1<br />

A320-100 150,796<br />

600 0.00<br />

2 A340-600 std 805,128<br />

1,000 0.00<br />

3 A340-600 std Belly 805,128<br />

1.000 0.00<br />

4 A380-800 1,239,000<br />

300 0.00<br />

5 B737-800 174,700<br />

2,000 0.00<br />

6 B747-400B Combi 877,000<br />

400 0.00<br />

7 B747-400ER Passenger 913,000<br />

300 0.00<br />

8 B757-300 273,500<br />

1,200 0.00<br />

9 B767-400 ER 451,000<br />

800 0.00<br />

10 B777-300 ER 777,000<br />

1,000 0.00<br />

11 B787-8 (Preliminary) 486,000<br />

600 0.00<br />

12 A340-200 std 568,563<br />

1,200 0.00<br />

13 A340-200 std Belly<br />

568,563 1,200 0.00<br />

Additional Airplane Information<br />

Subgrade CDF<br />

No.<br />

Name<br />

CDF<br />

Contribution<br />

CDF Max<br />

for Airplane<br />

P/C<br />

Ratio<br />

1<br />

A320-100 0.00<br />

0.00 1.21<br />

2 A340-600 std 0.05<br />

0.05 0.59<br />

3 A340-600 std Belly 0.00<br />

0.03 0.58<br />

4 A380-800 0.01<br />

0.01 0.42<br />

5 B737-800 0.00<br />

0.00 1.22<br />

6 B747-400B Combi 0.01<br />

0.01 0.57<br />

7 B747-400ER Passenger 0.01<br />

0.02 0.57<br />

8 B757-300 0.00<br />

0.00 0.73<br />

9 B767-400 ER 0.03<br />

0.05 0.60<br />

10 B777-300 ER 0.85<br />

0.85 0.40<br />

11 B787-8 (Preliminary) 0.03<br />

0.03 0.58<br />

12 A340-200 std 0.00<br />

0.00 0.59<br />

13 A340-200 std Belly<br />

0.00 0.00 1.17<br />

Figure 12.13 FAARFIELD summary Window: flexible-pavement example.

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