Journal of Advanced Transportation / 2019 / Article / Tab 2

Research Article

An Airfield Soil Pavement Design Method Based on Rut Depth and Cumulative Fatigue

Table 2

Partial parameters of A-type transport aircraft.

TypeMaximum mass during take-off (kN)Load distribution coefficient of main landing gearSingle-wheel load of main landing gear (kN)Tire pressure (MPa)Area of wheel tread (m2)Wheel tread width (m)Distance between wheel on the same side (S/m)Width of inner track between left and right main wheel (L/m)

A-type transport aircraft6200.95790.780.1110.27640.4904.43

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