Розрахунок динамічних параметрів підйомного комплексу амфібійних суден на повітряній подушці

Abstract

A mathematical model for simulation and designing of the hovercraft’s lifting complex has been developed. The mathematical model allows calculating the parameters of the hovercraft’s lifting complex in different modes of its operation. The equations presented in the models allow calculating the air pressure in both rigid and flexible receivers of the lifting complex, in the sections of the air cushion, as well as the required pressure of blowers. Furthermore, it is possible to determine the air flow rates in the bow, stern and side flexible receivers, as well as the air flow rate from air cushion sections to the atmosphere.