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The study of the influence of the gamma function on the flutter velocity

Most of the problems of hereditarily deformable systems, mathematically modeled by means of linear weakly singular integro-differential equations, are not linear in the strict approach. Linearization of such problems (both geometrically and physically, as well as aerodynamically) is performed solely in order to avoid mathematical difficulties associated with solving nonlinear integral and integro-differential equations. In this article, the aerodynamic profile of the ”hereditarily deformed” wing is considered in a steady flow of gas with different velocities and we investigate the parameters due to the dynamics of the process.