Abstract
In a previous paper (Meksyn 1948) the author gave a method of calculating the velocity distribution in a laminar boundary layer on cylindrical bodies. The aim of the present paper is to extend the method to the case of laminar boundary layers on bodies of revolution. The problem has been treated, so far, only in a few papers (Goldstein 1938, §§51, 52, 61). Millikan (1932) has derived boundary-layer equations and Kármán’s momentum equation for bodies of revolution, and, assuming a parabolic distribution for the velocity
u
in the laminar part, and
u ~ y
1/η
in the turbulent part (where
y
is the distance from the surface), he has applied the momentum equation to airship-line bodies. Fediaersky (1934) derived independently the momentum equation for bodies of revolution and applied it to airship-like bodies by assuming
u ~ u
n
, where
n
is arbitrary. Tomotika (1935) applied the momentum equation to the evaluation of various boundary-layer quantities for bodies of revolution, in particular for a sphere. Fage (1936) used Tomotika’s results to evaluate the surface friction at the forward part of a sphere. In the present paper the general boundary-layer equations are derived for axially symmetrical motions of bodies of revolution; the equations are partially solved for a sphere, and the results compared with Fage’s (1936) measurements.
Reference8 articles.
1. Fage A. 1936 Rep.Memor. Aero. Res.
2. Fediaevsky K. 1934 Trans. Central Aero-Hydrodyn. Inst. Moscow no. 179.
3. Goldstein S. 1938 M odem developments in fluid dynamics. Oxford: Clarendon Press.
4. On an equation occurring in Falkner and Skan's approximate treatment of the equations of the boundary layer
5. Lamb H. 1932 Hydrodynamics. Camb. Univ. Press.
Cited by
8 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献