摘要
在传统圆弧形风帆和NACA翼型的基础上,针对船用助航风帆的特点提出一种改进型的风帆翼型,利用Fluent软件,采用标准k-ε模型对传统圆弧形帆、NACA翼型和改进翼型在5-20 m/s、0-90°不同流速和不同攻角下翼型的空气动力特性进行了数值模拟计算,获得了相应的升力系数和阻力系数以及升阻比,证明其升力和阻升比均比传统圆弧形风帆有很大的提高.
On the basis of traditional arcing sail and NACA airfoil,an improved sail airfoil is proposed according to the characteristic of sail-assisted equipment. The dynamic characteristic of traditional arcing sails,NACA airfoil and proposed airfoil are simulated with Fluent software based on standard k- ε model for different wind directions from 0 to 90°and different wind velocity from 5m / s to 20 m / s. Lift coefficients,drag coefficients and lift-todrag ratio were calculated. The results of numerical simulation showed that the proposed airfoil sail had bigger lift force and lift-to-drag ratio than traditional arcing sails.
出处
《江苏科技大学学报（自然科学版）》
CAS
北大核心
2016年第4期323-327,共5页
Journal of Jiangsu University of Science and Technology:Natural Science Edition
基金
江苏省重点实验室开放研究基金资助项目(CJ1503)
江苏省自然科学基金青年基金资助项目(BK20160559)
关键词
圆弧形风帆
翼型风帆
升力系数
阻力系数
升阻比
traditional arcing sail
airfoil＇s sail
lift coefficient
drag coefficient
lift-to-drag ratio
