کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
761564 1462691 2015 15 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Dependence of turbulent wall-shear stress on the amplitude of spanwise transversal surface waves
ترجمه فارسی عنوان
وابستگی تنش برشی دیافراگمی بر دامنه امواج سطحی فرکانس تقطیر
کلمات کلیدی
کاهش کشیدن، امواج سفر متقاطع، شبیه سازی بزرگ
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مکانیک محاسباتی
چکیده انگلیسی


• Large-eddy simulations of turbulent boundary layer ow over spanwise traveling transversal waves are performed.
• Reynolds numbers based on the momentum thickness are Reθ = 2000, 5000, and 7000.
• The amplitudes of the waves are A+ = 30, 50, and 70.
• The maximum observed drag reduction is 11.4%.
• The results indicate that the friction drag above actuated surfaces does not scale in inner units.

Large-eddy simulations of turbulent boundary layer flow over a flat plate whose surface is actuated by spanwise traveling transversal waves are performed. Although it is known that moving surfaces can result in drag reduction compared to the non-actuated flow problem, it is an open question whether the drag reduction depends monotonically on the parameters defining the transversal wave of the surface, i.e., the amplitude A+A+ , the wavelength λ+λ+, and the period T+T+. It is the purpose of this study, to analyze the dependence of the drag reduction on the amplitude A+A+ in an extended Reynolds number range while the other wave parameters are kept constant. To be more precise, the analysis is based on the amplitudes A+=30A+=30, 50, and 70 and the Reynolds numbers based on the momentum thickness Reθ = 2000, 5000, and 7000. The results show that the drag reduction decreases at increasing Reynolds number. The maximum drag reduction is 11.4%. Furthermore, independently from the Reynolds number the local wall-shear stress is lowered at higher wave amplitude. However, the analysis of the drag reduction, which is defined by the wall-shear stress integrated over the surface area, evidences an optimum amplitude to exist due to the variation of the area as a function of the amplitude. This is shown for Reθ = 2000, where the drag reduction for A+=50A+=50 is higher than for A+=30A+=30 and A+=70A+=70. The results further indicate that unlike for flows over non-actuated surfaces the friction drag above actuated surfaces no longer scales in inner units.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Computers & Fluids - Volume 119, 22 September 2015, Pages 261–275
نویسندگان
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