A numerical study of low reynolds number fluid-structure interaction

1989 ◽  
Vol 3 (1) ◽  
pp. 37-60 ◽  
Author(s):  
S. Moorty ◽  
M.D. Olson
2013 ◽  
Vol 387 ◽  
pp. 241-245
Author(s):  
Zeng Qiang Qiao ◽  
Yong Bo Yang

The quality and dependability of the small unmanned plane is more and more important currently. For the small unmanned plane under the conditions of Low-Reynolds, the air viscosity has relatively greater influence on its aerodynamic performance. This is one of the greatest difficulties to design a small unmanned plane. The aerodynamic performance of bionic aerofoil and NACA 4412 is contrastively analyzed while the Reynolds-Number is and by the Fluent. The computational result and the analysis show that the fluid-structure interaction is an important issue to consider while designing the small unmanned plane.


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