Unsteady Boundary Layer near the Forward Stagnation Point with Uniform Suction or Injection
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概要
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This paper is concerned with the numerical investigation of the two-dimensional unsteady incompressible boundary layer near the forward stagnation point of an infinite plane wall, with uniform suction or injection through the wall. The velocity of the external flow as well as that of suction or injection is assumed to be kept constant in time t after their impulsive start from rest at t=0. Since the governing equation for the present problem proves to be non-similar, an attempt to solve it is made by employing the difference-differential method, together with the iterative scheme in solving the resulting differential equations. Numerical results are given for the velocity profile, skin friction, displacement thickness and momentum thickness.
- 社団法人日本物理学会の論文
- 1971-09-05
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