Subsonic compressible flow in two-sided lid-driven cavity. Part I: Equal walls temperatures

• Published in: International journal of heat and mass transfer Vol. 50; no. 21; pp. 4206 - 4218
• Main Authors: Shah, P., Rovagnati, B., Mashayek, F., Jacobs, G.B.
• Format: Journal Article
• Language: English
• Published: Oxford Elsevier Ltd 01.10.2007; Elsevier
• Subjects: Compressible flows; shock and detonation phenomena; Computational methods in fluid dynamics; Exact sciences and technology; Fluid dynamics; Fundamental areas of phenomenology (including applications); General subsonic flows; Laminar flows; Laminar flows in cavities; Physics; Compressible fluid; Streamlines; Subsonic flow; Chebyshev polynomial; Digital simulation; Boundary conditions; Modelling; Aspect ratio; Cavity flow; Viscous fluids; Discretization method; Moving wall
• ISSN: 0017-9310; 1879-2189
• DOI: 10.1016/j.ijheatmasstransfer.2007.02.028

This paper presents a numerical study of the laminar, viscous, subsonic compressible flow in a two-dimensional, two-sided, lid-driven cavity using a multi-domain spectral element method. The flow is driven by steadily moving two opposite walls vertically in opposite directions. All the bounding walls have equal temperatures. The results of the simulations are used to investigate the effects of the cavity aspect ratio, the Reynolds number and the Mach number on the flow. At lower Reynolds numbers, the flow pattern consists of two separate co-rotating vortices contiguous to the moving walls. For higher Reynolds numbers, initially a two-vortex flow is formed, which eventually turns into a single elliptical vortex occupying most of the cavity. For a higher aspect ratio, the flow patterns are dissimilar in that the streamlines become more and more elliptic. For aspect ratios as high as 2.5, at high Reynolds numbers, a three-vortex stage is formed. It is found that the compressibility effects are not very significant for Mach numbers less than 0.4. Dissipation of kinetic energy into internal energy changes the temperature field especially near the boundaries. Boundary layer studies suggest that the velocity and temperature boundary layer thicknesses are lower for higher Reynolds numbers. For engineering purposes, these thicknesses can be approximated by the existing flat-plate solutions.