Computation of the two-dimensional flow in a laminar boundary layer (1935)
NASA Technical Reports Server (NTRS) · leaf 7
lhausen's solution, where it is £■=0, the front stagnation point. Because U=0 at applicable. Unfortunately, all of the satisfactory x=0, we find here a singularity; there is no true bound- exact solutions are cases in which X is positive and ary layer right at the stagnation point. The isocline… … x Fiqube 5.—Isocline diagram for boundary layer of a cylinder the attempt to construct the solution curve leads imme- 0.8 1.2 1.6 0.4 2.0 24 diately to the singular point. Fioube 6.—Velocity distribution In boundary layer of cylinder at two distances It may be shown that the zero isocline leaves…
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