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- W967492776 abstract "This chapter briefly discusses the external flows. Flow around a body placed in a uniform flow develops a thin layer along the body surface with largely changing velocity, which is the boundary layer, due to the viscosity of the fluid. Furthermore, the flow separates behind the body, discharging a wave with eddies. Whenever a body is placed in a flow, the body is subject to a force from the surrounding fluid. When a flat plate is placed in the flow direction, it is only subject to a force in the downstream direction. Thereafter, a drag is produced because a streamline separates behind a body, develops vortices, and lowers its pressure. Therefore, in order to reduce the drag, it suffices to make the body into a shape from which the flow does not separate. This is called the streamline shape. Of the forces acting on a body placed in a flow, if the body is manufactured as to make the lift larger than the drag, it is called a wing, airfoil, or blade. The shape of a wing section is called an airfoil section." @default.
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- W967492776 date "1998-01-01" @default.
- W967492776 modified "2023-09-27" @default.
- W967492776 title "Drag and lift" @default.
- W967492776 doi "https://doi.org/10.1016/b978-034067649-3/50011-7" @default.
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