In this panel, it is possible to take into account the possible presence of surcharges.
The software allows for the consideration of the presence of loads:
•uniformly distributed
•in strips
•linear
In the case of uniformly distributed loads, the thrust increment due to the load is calculated by multiplying the load intensity by the coefficient of active thrust Ka. In the case of a strip load or linear load, the thrust increment is calculated using solutions derived from the theory of elastic half-space.