On motion of fluid in boundary layer near line of intersection of two planes /
by L.G. Loitsianskii and V.P. Bolshakov.

Description

Main Author

Loĭt�si�anskiĭ, L. G. (Lev Gerasimovich)

Related Names

Bolshakov, V. P.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : NACA, 1951.

Subjects

Laminar boundary layer.
Aerodynamics.

Summary

A motion of a slightly viscous incompressible fluid that flows between two semi-infinite planes which intersect at an angle between 0À and 180À is discussed. The increase in thickness of the boundary layer near the line of intersection of the two planes, the limits of the effect of the corner, and the effect on the drag are determined. The analysis is made for both laminar and turbulent flow by using the momentum theorem and assuming suitable velocity profiles.

Note

"Translation of "O dvizhenii zhidkosti v pogranichnom sloe vblizi linii peresechenia dvukh ploskostei." Rep. No. 279, CAHI, 1936."
"Report date November 1951."
Also available in electronic format.

Physical Description

26 p. : ill. ; 27 cm.

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