| Аннотацiя: | Modern ideology of computational approaches for solving initial value problems of continuum mechanics is based on the creation of an adequate mathematical models and computational methods of construction based on the geometric shape of the object. For the purpose of numerical implementation of the method of boundary integral equations developed algorithmic process coordinate surfaces perspective bearing systems of arbitrary spatial form in order to further their triangulation, ensuring the correct conduct of computer simulation to determine the distributed and the total aerodynamic characteristics. |
