Flow characteristics and flow-induced forces of a stationary and rotating triangular cylinder with different incidence angles at low Reynolds numbers

In this paper, the problem of two-dimensional fluid flow past a stationary and rotationally oscillating equilateral triangular cylinder with a variable incident angle, Reynolds number, oscillating amplitude, and oscillating frequency is numerically investigated. The computations are carried out by using a two-step Taylor-characteristic-based Galerkin (TCBG) algorithm. For the stationary cases, simulations are conducted at various incident angles of alpha=0.0-60.0 degrees and Reynolds numbers of Re=50-160. For the oscillation cases, the investigations are done at various oscillating amplitudes of theta(max)=7.5-30.0 degrees and oscillating frequencies of F-s/F-o=0.5-3.0 considering two different incidence angles (alpha=0.0 degrees, 60.0 degrees) and three different Reynolds numbers (Re=50, 100, 150). The results show that the influences of key parameters (incidence angle, Reynolds number, oscillating amplitude, and oscillating frequency) are significant on the flow pattern and hydrodynamic forces. For the stationary cases, at smaller angle of incidence (alpha <= 30.0 degrees), Reynolds number has a large impact on the position of the separation points. When a is between 30.0 degrees and 60.0 degrees, it was found that the separation points are located at the rear corners. From a topological point of view, the diagram of flow pattern is summarized, including two distinct patterns, namely, main separation and vortex merging. A deep analysis of the influence of Reynolds number and incidence angles on the mean pressure coefficient along the triangular cylinder surface is presented. Additionally, for the oscillating cases, the lock-on phenomenon is captured. The dominant flow patterns are 2S mode and P+S mode in lock-on region at alpha=0.0 degrees. It is found at alpha=60.0 degrees, however, that the flow pattern is predominantly 2S mode. Furthermore, except for the case of F-s/F-o=2.0, the mean drag decreases as the oscillating amplitude increases for each Reynolds number at alpha=0.0 degrees. At alpha=60.0 degrees, the minimum mean drag for F-s/F-o=1.5 is lower than that for stationary case, and occurs at theta(max)=15.0 degrees (Re=100) and theta(max)=22.5 degrees (Re=150), respectively. Finally, the effect of Reynolds number on a rotational oscillation cylinder is elucidated. (C) 2013 Elsevier Ltd. All rights reserved.