A Note on the Laminar Boundary Layer on a Circular Cylinder in Axial Incompressible Flow
Howard R. Kelly · Journal of the aeronautical sciences. [REQUEST TITLE] · 1954
£ = ( 4 / C ) V J « M (2) In a later paper, Eckert mentioned that Seban and Bond obtained no clear results because of the limited number of terms in the series expansion.'.' I t is felt by the present writer that the series in £ should converge rapidly for £< C 1.0, but tha t the results in Eq. (1) are in error for another reason, as will be shown. The authors of reference 1 define a displacement thickness by the equation