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Simulation of Flows Near Wings with Supersonic Edgesстатья
- Автор: Maksimov F.A.
- Сборник: Advances in Theory and Practice of Computational Mechanics. Smart Innovation, Systems and Technologies
- Том: 274
- Глава в коллективной монографии
- Год издания: 2022
- Издательство: Springer Singapore
- Местоположение издательства: Singapore
- Первая страница: 87
- Последняя страница: 103
- Номер статьи: 7
- Аннотация: Options for constructing a grid with an edge selection and setting the conditions for the conicity of the flow relative to the edge are offered to simulate the flow around conical bodies with a sharp supersonic edge. Methods for constructing a grid near a star-shaped body, a flat and V- or Λ-shaped wing, near a wing with a central body, and a V-shaped wing with a leading edge of negative sweep have been implemented. The boundary condition for the flow conicity relative to the edge is sufficient for constructing a solution. Calculations of the flow around several variants of geometries of bodies of various types with a fixed midsection area and wing span are carried out, their aerodynamic characteristics are compared.
- Добавил в систему: Максимов Федор Александрович