Unsteady Boundary Layer Flows past an Impulsively Started Circular Cylinder
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概要
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The two-dimensional unsteady flow of an incompressible viscous fluid around a circular cylinder, which is started impulsively from rest, is considered. Numerical solutions of unsteady boundary-layer equation are sought by employing the local non-similarity solution method presented by Sparrow, Quack and Boerner (Amer. Inst. Aero. Astronaut. J. 8 (1970) 1936), together with the difference-defferential method. Numerical solutions are given for the velocity profile, wall shear and the time when the separation of the boundary layer occurs; the development of the boundary layer and its separation are discussed.
- 社団法人日本物理学会の論文
- 1976-04-15
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