Table 9 The maximum bending tensile stress at the bottom of the track slab under the dynamic load of the aircraft(MPa).
Frost heave (mm) | B767- 300ER | B747-400 | A380-800 |
---|---|---|---|
10 | 1.922 | 3.337 | 4.043 |
15 | 2.072 | 4.213 | 4.957 |
20 | 2.265 | 5.063 | 5.974 |
25 | 2.484 | 5.854 | 6.690 |