ARTÍCULO
TITULO

Numerical Investigation of Vortex Shedding from a 5:1 Rectangular Cylinder at Different Angles of Attack

Jian Wu    
Yakun Liu    
Di Zhang    
Ze Cao and Zijun Guo    

Resumen

Although flow around a 5:1 rectangular cylinder at small angles of attack (AoA) has been extensively studied, when the AoA becomes larger, the research is rare. Therefore, this study performs Unsteady Reynolds-Averaged Navier-Stokes simulations (URANS) using the k-? SST turbulence model for unsteady flow around a two-dimensional 5:1 rectangular cylinder at different AoAs up to 45°. A strong dependence of the flow characteristics on AoA is observed through the analysis of the time-averaged lift coefficient, drag coefficient, and Strouhal number. The peak of lift and drag coefficient is observed to be correlated, respectively, to the leading- and trailing-edge vortex based on the analysis of the flow. The x'-directional length of the main recirculation bubble on the top side and the distance from the bubble center to the leading edge of the cylinder both reach the maximum when a = 15°. In addition, the standard deviation σx′" role="presentation">????'sx' s x ' of the time-averaged velocity U¯x′" role="presentation">???????????'U¯x' U ¯ x ' along the cylinder shows a trend of increasing at first and then decreasing, and that σy′" role="presentation">????'sy' s y ' also shows the same trend at a = 20°~45°; it fluctuates within a range of 0.05~0.2 at a = 0°~20°. Finally, two principal modes of vortex shedding are observed with a = 15° being their turning point, (i) ?1 + 1? mode: in one vortex shedding period, two major vortices shed off from the top and bottom sides of the cylinder at a = 15°; (ii) ?2 + 2? mode, four vortices shed off from the top and bottom sides of the cylinder at a > 15° in one vortex shedding period.

 Artículos similares

       
 
Wenjie Shen, Suofang Wang, Mengyuan Wang, Jia Suo and Zhao Zhang    
Improving airflow pressure is of great significance for the cooling and sealing of aeroengines. In a co-rotating cavity with radial inflow, vortex reducers are used to decrease the pressure drop. However, the performance of traditional vortex reducers is... ver más
Revista: Aerospace

 
Panagiotis D. Kordas, George N. Lampeas and Konstantinos T. Fotopoulos    
The main purpose of this study comprises the design and the development of a novel experimental configuration for carrying out tests on a full-scale stiffened panel manufactured of fiber-reinforced thermoplastic material. Two different test-bench design ... ver más
Revista: Aerospace

 
Junyao Zhang, Hao Zhan and Baigang Mi    
The submerged inlet exhibits good stealth characteristics and lower drag, but it has a low total pressure recovery coefficient and high distortion rate, which limits its widespread application. This paper proposes a vortex diverter aimed at enhancing the... ver más
Revista: Aerospace

 
Shuang Ruan, Ming Zhang, Shaofei Yang, Xiaohang Hu and Hong Nie    
A dynamic model is established to investigate the shimmy instability of a landing gear system, considering the influence of nonlinear damping. The stability criterion is utilized to determine the critical speed at which the landing gear system becomes un... ver más
Revista: Aerospace

 
Mengxiang Li, Guo Wang, Kun Liu, Yue Lu and Jiaxia Wang    
The safety assessment of ship cargo securing systems is of significant importance in preventing casualties, vessel instability, and economic losses resulting from the failure of securing systems during transportation in adverse sea conditions. In this st... ver más