Abstract
This chapter discusses the steady incompressible laminar flow separation on bodies of revolution and other three-dimensional solid configurations. The problem of flow separation on axial symmetric bodies is closely correlated with that one on a two-dimensional body, but the flow separation on a three-dimensional body is general and difficult to solve. For particular cases, however, the solutions are known. The chapter presents several available analyses of the laminar separation. The prediction of laminar separation for the arbitrary three-dimensional flow is complex due to crossflow. The results of three-dimensional boundary layer show that the boundary layer becomes thin with acceleration but becomes thick with deceleration. The chapter highlights the laminar flow separation on a body of revolution and a delta wing that includes Maogler's transformation, Laminar separation on a yawed cylinder, Lammar separation on cone at angles of attack, and the separation of flow on a delta wing.
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