کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
857126 1470727 2015 7 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Optimization of Suction Control on an Airfoil Using Multi-island Genetic Algorithm
ترجمه فارسی عنوان
بهینه سازی کنترل مکش بر روی یک هواپیما با استفاده از الگوریتم ژنتیک چند جزیره
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی (عمومی)
چکیده انگلیسی

To overcome the disadvantage of large suction requirements, the suction control for drag reduction is optimized. Computational fluid dynamics (CFD), in conjunction with multi-island genetic algorithm (MIGA), is employed to achieve the optimization. An E387 airfoil is employed as the physical model. The suction location and mass flux of a slot are set as the design parameters. The goal is to minimize both the airfoil drag and suction requirement by identifying the optimal suction location on the upper airfoil surface. The effects of different numbers of suction slots were investigated. Results show that the suction control for drag reduction could be optimized using MIGA. For a single-suction slot, the reduction in airfoil drag is up to 8.3%, and the mass flux of a slot reaches the lower limit of the optimization interval. The increase in suction slot number results in a better drag reduction effect, which is accompanied by larger suction requirement and slower convergence. The main reason for airfoil drag reduction is the decrease in the pressure drag.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Procedia Engineering - Volume 99, 2015, Pages 696-702