کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
8065571 | 1520693 | 2015 | 9 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Vortex-induced vibration on a two-dimensional circular cylinder with low Reynolds number and low mass-damping parameter
ترجمه فارسی عنوان
لرزش ناشی از وایبر در یک سیلندر دایره ای دو بعدی با تعداد رینولدز کم و پارامتر کم جرم
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی دریا (اقیانوس)
چکیده انگلیسی
The vortex induced vibration (VIV) on a circular cylinder with low mass-damping parameter and low Reynolds number is investigated numerically as basis for applications on dynamics of risers used in the offshore oil and gas industry and as a first step before tackling the harder high Reynolds number problem. The cylinder is supported by a spring and a damper and free to vibrate in the transverse direction. The numerical solution of the Unsteady Reynolds-Averaged Navier-Stokes equations written in curvilinear coordinates is obtained using an upwind and Total Variation Diminishing conservative scheme and the k-ε turbulence model. Results were obtained for the phase angle, response amplitude, response frequency, and lift coefficient for reduced velocities from 2 to 12, for six different fixed Reynolds numbers, and for three different proportional variations of Reynolds number with reduced velocity, 2000-6000, 2000-12,000, and 2000-24,000. The results indicate the strong effect of the Reynolds number on the response amplitude, lift coefficient, and response frequency for a low mass-damping parameter. The upper branch of the response amplitude curve is only obtained when the Reynolds number varies proportionally to reduced velocity. For a fixed Reynolds number, only the initial and lower branches are captured.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Ocean Engineering - Volume 97, 15 March 2015, Pages 156-164
Journal: Ocean Engineering - Volume 97, 15 March 2015, Pages 156-164
نویسندگان
Juan B.V. Wanderley, Luiz Felipe N. Soares,