| Abstract: | ![]()
A theory of the flow around slender conical bodies with a star-shaped cross-section in regimes with shock attachment along the length of the leading edges is developed. The aerodynamic characteristics of the slender star body, a single cycle of which represents a V-shaped wing, are obtained for different numbers of reflections of the disturbances proceeding from the leading edges of the cycles from the wing cantilevers, using superposition of the solutions of linear problems of flow around the V-wing. |
