Options
Die inkompressible Grenzschicht höherer Ordnung am rotationssymmetrischen Staupunkt bei starkem Absaugen oder Ausblasen
Date Issued
01-05-1973
Author(s)
Rajappa, Nanguneri R.
Abstract
The incompressible laminar second-order boundary layer at an axisymmetric stagnation point with suction or injection is investigated. The effects of curvature and displacement on wall shear stress and heat transfer are given as functions of the suction or injection parameter. For the limiting cases of strong suction or injection asymptotic formulae have been developed. © 1973 Birkhäuser Verlag.
Volume
24