

LAMINAR BOUNDARY LAYER WITH FAVORABLE PRESSURE GRADIENT ON THE UNIFORMLY HEATED SURFACE
Sakhnov A.Yu.
Institute of Thermophysics SB RAS, Novosibirsk, Russia
Citation:
Sakhnov, A.Yu., (2013) Laminar boundary layer with favorable pressure gradient on the uniformly heated surface, Modern Science: Researches, Ideas, Results, Technologies, Iss. #1(12), PP. 220  224.

Keywords: boundary layer; favorable pressure gradient; temperature factor 
Abstracts:
The results of numerical research of accelerated flow on heated flat plate with constant temperature are presented in the work. It is shown simultaneous influence of favorable pressure gradient and nonisothermal conditions on a boundary layer leads to increasing of skinfriction coefficient and Stanton number in relation to accelerated quasiisothermal boundary layer. At this, velocity and temperature profiles become more filled. In the case of considerable acceleration of the flow and significant heating of the wall the velocity profile is deformed next way: the velocity in the boundary layer become higher than that in the potential flow. The deformation of longitudinal velocity profile in laminarized flow can be over 20 %. It is suggested a simple analytical formula for calculation of skinfriction coefficient in asymptotic flow. The formula takes into account simultaneously influence of favorable pressure gradient and temperature factor. 
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