Characterization of Lip Thickness Effects in Subsonic Coaxial Jets with Varying Velocity Ratio
- سال انتشار: 1404
- محل انتشار: دوماهنامه مکانیک سیالات کاربردی، دوره: 18، شماره: 10
- کد COI اختصاصی: JR_JAFM-18-10_006
- زبان مقاله: انگلیسی
- تعداد مشاهده: 27
نویسندگان
Department of Aeronautical Engineering, Vel Tech Rangarajan Dr. Sagunthala R&D Institute of Science and Technology, Avadi, Tamil Nadu, ۶۰۰۰۶۲, India
Department of Aeronautical Engineering, Vel Tech Rangarajan Dr. Sagunthala R&D Institute of Science and Technology, Avadi, Tamil Nadu, ۶۰۰۰۶۲, India
Department of Aeronautical Engineering, Nehru Institute of Engineering and Technology, Coimbatore, Tamil Nadu, ۶۴۱۱۰۵, India
Department of Aeronautical Engineering, KIT – Kalaignarkarunanidhi Institute of Technology, Coimbatore, Tamil Nadu, ۶۴۱۴۰۲, India
Department of Aeronautical and Aerospace Engineering, KCG College of Technology, Chennai, Tamil Nadu, ۶۰۰۰۹۷, India
Department of Aerospace Engineering, Indian Institute of Technology - Kanpur, Kanpur, Uttar Pradesh, ۲۰۸۰۱۶, India
چکیده
This study aims to investigate the influence of lip thickness and velocity ratio on the mixing characteristics of coaxial jets. The primary objective is to examine and compare the flow behavior of thin and thick lip coaxial nozzles at various velocity ratios, using both experimental and numerical methods. The scope of the work focuses on identifying critical lip thicknesses ranging from ۰.۷ mm to ۱۰.۷ mm, in increments of ۲ mm. The primary jet exit Mach number is maintained at ۰.۶, while the secondary jet Mach number is varied from ۰% to ۱۰۰% of the primary jet velocity. Numerical simulations are performed using a validated turbulence model to understand the flow physics, such as potential core variation and jet interaction mechanisms. In this research, the Reynolds number vary from ۰ to ۱.۶۲x۱۰۵ and the turbulence intensity has a minimum value for a ۴ and it reaches to ۴.۹ at maximum. The results show that in thin lip nozzles, the increase in velocity ratio extends the potential core length due to dominant shear layer interaction. In contrast, thick lip nozzles display reduced core length with increasing velocity ratio, primarily due to wake region interaction. Among the cases studied, the ۱۰.۷ mm lip thickness configuration exhibits superior mixing characteristics, indicating the presence of a critical lip geometry for enhanced performance. These findings provide insight into optimizing coaxial jet design for applications requiring efficient mixing.کلیدواژه ها
Thin lip, Thick lip, Velocity ratio, Shear dominant, Wake dominantاطلاعات بیشتر در مورد COI
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