کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
5017473 1466576 2017 17 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
On the effects of tip deflection in flapping propulsion
ترجمه فارسی عنوان
در اثر انحراف نوک در حرکت موشک
کلمات کلیدی
نیروی محرکه بیوژنتیک، فلاپینگ، شنا کردن، بیدار می شود
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی مکانیک
چکیده انگلیسی
Experiments have been performed with a flapping system that allows to set different inclinations to the tip of a robotic fin. Direct force measurements and Digital Particle Image Velocimetry (DPIV) have been used to study the propulsive performance for the different tip configurations investigated. The effects of the geometry of the tip and the kinematics imposed to the fin on the impulse generated, are discussed in detail. We show how the capacity of the system to produce impulse can be altered by imposing certain tip geometries that imply small local changes of the trailing edge. The modified tip geometries are closely related to the way vortices evolve in the near wake region and therefore how momentum is transferred to the wake. We have found that the configurations that produce the highest impulses have the tip deflected to the suction side of the system while flapping. The dynamic control of the tip allows changes in the impulse generated.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Journal of Fluids and Structures - Volume 71, May 2017, Pages 217-233
نویسندگان
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