Boundary layer flow of air past solid surfaces in the presence of rainfall
The steady two-dimensional laminar flow of an air stream, flowing past a solid surface at high Reynolds number, is examined in the presence of rainfall. As raindrops sediment on the surface they coalesce and form a continuous water film that flows due to shear, pressure drop and gravity, in general....
Gespeichert in:
Veröffentlicht in: | Journal of fluid mechanics 2000-12, Vol.425, p.79-110, Article S0022112000002081 |
---|---|
Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | The steady two-dimensional laminar flow of an air stream, flowing past a solid surface
at high Reynolds number, is examined in the presence of rainfall. As raindrops
sediment on the surface they coalesce and form a continuous water film that flows
due to shear, pressure drop and gravity, in general. In the limit as the boundary
layer and film thickness remain smaller than the radius of curvature of the surface a
simplified lubrication-type formulation describes the flow field in the film, whereas the
usual boundary layer formulation is applied in the gas phase. In the case of a flat plate
and close to the leading edge, x → 0, a piecewise-self-similar solution is obtained,
according to which creeping flow conditions prevail in the film and its thickness
grows like x3/4, whereas the Blasius solution is recovered in the air stream. Numerical
solution of the governing equations in the two phases and for the entire range of
distances from the leading edge, x = O(1), shows that the film thickness increases as
the rainfall rate, r˙, increases or as the free-stream velocity,
U∞, decreases and that
the region of validity of the asymptotic result covers a wide range of the relevant
problem parameters. In the case of flow past a NACA-0008 airfoil at zero angle
of attack a Goldstein singularity may appear far downstream on the airfoil surface
due to adverse pressure gradients, indicating flow reversal and eddy formation inside
the liquid film, and, possibly, flow separation. However, when the effect of gravity
becomes evident in the film flow, as the Froude number decreases, and provided
gravity acts in such a way as to negate the effect of the adverse pressure gradient,
the location of the singularity is displaced towards the trailing edge of the airfoil and
the flow pattern resembles that for flow past a flat plate. The opposite happens when
gravity is aligned with the adverse pressure gradient. In addition it was found that
there exists a critical water film thickness beyond which the film has a lubricating
effect delaying the appearance of the singularity. Below this threshold the presence of
the liquid film actually enhances the formation of the singularity. |
---|---|
ISSN: | 0022-1120 1469-7645 |
DOI: | 10.1017/S0022112000002081 |