This work presents a simulation of a hexagonal membrane. Some partial solutions for the problem of free vibrations of a membrane of regular hexagonal shape with a different initial bending of the surface are obtained and the natural frequencies of vibrations are found. The result obtained can be used in modeling wing structures in the form of a hexagon of such aircraft as a paraglider.
Keywords: Modeling of a hexagonal wing, free vibrations of a membrane, a membrane of a regular hexagonal shape, natural frequencies of vibrations