ABSTRACT. The forced convective flow and heat transfer of nanofluids past a rotating cylinder placed in a uniform cross stream is investigated numerically. The computations are carried out at a representative Reynolds number (Re) of 200. The dimensionless cylinder rotation rate (α) is varied between 0 and 6. The range of nanoparticle volume fractions (φ) considered is 0 ≤ φ ≤ 5%. Two-dimensional and unsteady mass continuity, momentum, and energy equations have been discretized using finite volume method. SIMPLE algorithm has been applied for solving the pressure linked equations. The effect of rotation rates (α) on fluid flow and heat transfer were investigated numerically. In addition, time-averaged (lift and drag coefficients and Nusselt number) results were obtained and compared with the literature data. A good agreement was obtained for both the local and averaged values.
INTRODUCTIONThe classical problem of viscous incompressible flow over a circular cylinder confined in a channel is one of the most widely studied problems in computational fluid dynamics (CFD). This type of flow problems frequently arise in various engineering fields. Because of its popularity, a plethora of numerical, theoretical and experimental results are available for this problem in the literature. . An explicit pseudo-spectral technique was adopted for resolving the fundamental equations. According to their results, when α = 3.25 more than one vortex is shed downstream. Kang [3] also has contributed significant work to this research area. Sequential numerical simulations at Re equal to 40, 60, 100 and 160 in the range of 0 ≤ α ≤ 2.5 were performed. It was observed that at 60 ≤ Re ≤ 160 the maximum value of a, which favors flow instability, varies logarithmically when plotted against Re. Zdravkovich [4], has compiled almost all the experimental, analytical and numerical simulation data on flow past cylinders,In the study of wake dynamics, bluff body rotation has always drawn considerable attention largely due to its effects on boundary layer separation and the Magnus effect. Increase in the lift magnitude more than classic Prandtl's limit due to increase in rotation rate of the circular cylinder was proposed by Glauart [5]. For the similar flow configuration, Kang and Choi [6], followed with the numerical solution of the unsteady governing equations in the primitive variables velocity and pressure for flows with Re = 60, 100 and 160 with 0 = α = 2.5. Their results showed that vortex shedding vanishes when α increases beyond a critical value which follows a logarithmic dependence on the Reynolds number (e.g., the critical dimensionless rotation rate α = 1.9 for Re = 160). Later, the work of (Mittal & Kumar, [7]) performed a comprehensive numerical investigation by fixing a moderate value of Re = 200 while considering a wide interval for the dimensionless rotation rate of 0 ≤ α ≤ 5. They used the finiteelement method to solve the unsteady incompressible Navier-Stokes equations in two-dimensions for the primitive variables velocity and ...