4.5 Article

Numerical analysis of heaving flexible airfoils in a viscous flow

期刊

AIAA JOURNAL
卷 44, 期 11, 页码 2773-2779

出版社

AMER INST AERONAUT ASTRONAUT
DOI: 10.2514/1.21203

关键词

-

向作者/读者索取更多资源

A numerical model for two-dimensional unsteady viscous fluid flow around flexible bodies is used to analyze the effect of chordwise flexibility on heaving airfoils. Flexible airfoils proved to be more efficient than the rigid ones. Both the output power and the input power increase in the flexible cases. The gain in efficiency is realized as a result of the output power increasing more than the input power. The density of the airfoils was shown to be a key factor in determining efficiency and power. In the parameter range analyzed, heavier airfoils are shown to generate less output power and to require proportionately less input power. Thus, heavier airfoils are more efficient than lighter airfoils. In the numerical model the bodies are represented by a distributed body force in the Navier-Stokes equations. The main advantage of this method is that the computations can be effected on a Cartesian grid, without having to fit the grid to the body surface. This approach is particularly useful when applied to the case of multiple bodies moving relative to each other, as well as flexible bodies, in which case the surface of the object changes dynamically.

作者

我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。

评论

主要评分

4.5
评分不足

次要评分

新颖性
-
重要性
-
科学严谨性
-
评价这篇论文

推荐

暂无数据
暂无数据