Effect of Guide Vane on Turbulence Characteristics for Single-Phase Flow through a ۹۰-Degree Pipe Bend

Publish Year: 1400
نوع سند: مقاله ژورنالی
زبان: English
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شناسه ملی سند علمی:

JR_JAFM-14-4_018

تاریخ نمایه سازی: 8 دی 1400

Abstract:

The present study expresses the turbulent flow characteristics through a ۹۰° pipe bend using a numerical ‎method by determining the solutions for Reynolds Averaged Navier-Stokes (RANS) expression using the k-ω ‎‎(SST) turbulence model. For that purpose, numerical analysis has been carried out by solving RANS equations ‎using ANSYS FLUENT ۱۶.۲, considering incompressible fluid in turbulent flow conditions. Simulations have ‎been carried out for three different Reynolds number ranging from ۱×۱۰۵ to ۱۰×۱۰۵ at three different bend ‎curvature ratios (Rc/D = ۱, ۱.۵, and ۲). Pipe bends with guide vane are generally used where flow separation ‎and space problem makes an issue in mechanical design. The presence of guide vane inside the bend ‎positively suppressed the flow separation and presence of cross-flow which can cause the engine to run off ‎design, thus reducing the engine efficiency. So, to observe the effect of guide vane and its position on ‎turbulence characteristics, four different positions of guide vane inside the bend are considered in the present ‎study. At first, an analysis was led to make sure that the results obtained from the present numerical model are ‎reliable and in line with previous results obtained from similar published experiments and numerical work. ‎Research has been conducted to find out the impact of Reynolds number, bend curvature ratio and position of ‎guide vane on different turbulence characteristics namely; turbulent kinetic energy, turbulent intensity, and ‎wall shear stress at bend outlet position. In general, the turbulent intensity is found larger for the lower bend ‎curvature ratio at the inner wall curvature side. Results for turbulent kinetic energy have similarities in results ‎with turbulent intensity. Significantly, the wall shear stress represented a strong dependency on the ‎circumferential angle at the bend outlet cross-section, and curvature ratio rather than Reynolds number and ‎guide vane positions‎‎.

Authors

S. Kumar Saha

Department of Aerospace Engineering & Applied Mechanics, Indian Institute of Engineering Science and ‎Technology, Shibpur, Howrah-۷۱۱۱۰۳, India‎

N. Nandi

Department of Aerospace Engineering & Applied Mechanics, Indian Institute of Engineering Science and ‎Technology, Shibpur, Howrah-۷۱۱۱۰۳, India‎