Developing Laminar Gravity-Driven Thin Liquid Film Flow Down an Inclined Plane
Three-dimensional (3D)-steady-developing-laminar-isothermal-and gravity-driven thin liquid film flow adjacent to an inclined plane is examined and the effects of film flow rate, surface tension, and surface inclination angle on the film thickness and film width are presented. The film flow was numerically simulated using the volume of fluid model and experimental verification was conducted by measuring film thickness and width using a laser focus displacement instrument. The steady film flow that is considered in this study does not have a leading contact line, however, it has two steady side contact lines with the substrate surface at the outer edge of its width. Results reveal that the film width decreases and the average film thickness increases as the film flows down the inclined plane. The film thickness and width decrease but its streamwise velocity increases as surface inclination angle (as measured from the horizontal plane) increases. A higher film flow rate is associated with a higher film thickness, a higher film width, and a higher average film velocity. Films with higher surface tension are associated with a smaller width and a higher average thickness. A ripple develops near the side contact line, i.e., the spanwise distribution of the film thickness exhibits peaks at the outer edges of the film width and the height of this ripple increases as the surface tension or the film flow rate increases. The width of the film decreases at a faster rate along the streamwise direction if liquid film has higher surface tension. Measurements of the film thickness and the film width compare favorably with the numerically simulated results. Copyright © 2010 by ASME.
H. Lan et al., "Developing Laminar Gravity-Driven Thin Liquid Film Flow Down an Inclined Plane," Journal of Fluids Engineering, Transactions of the ASME, American Society of Mechanical Engineers (ASME), Jan 2010.
The definitive version is available at http://dx.doi.org/10.1115/1.4002109
Mechanical and Aerospace Engineering
Article - Journal
© 2010 American Society of Mechanical Engineers (ASME), All rights reserved.