Effect of pre-strain and excess length on unsteady fluid-structure interactions of membrane airfoils

被引:89
作者
Rojratsirikul, P. [1 ]
Wang, Z. [1 ]
Gursul, I. [1 ]
机构
[1] Univ Bath, Dept Mech Engn, Bath BA2 7AY, Avon, England
关键词
Membrane; Vortex; Low Reynolds number flows; NONSLENDER DELTA-WINGS; AERODYNAMIC COEFFICIENTS; ELASTIC MEMBRANE; FLOW-CONTROL; AIR;
D O I
10.1016/j.jfluidstructs.2010.01.005
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Aerodynamic characteristics of two-dimensional membrane airfoils were experimentally investigated in a wind tunnel. The effects of the membrane pre-strain and excess length on the unsteady aspects of the fluid structure interaction were studied. The deformation of the membrane as a function of angle of attack and free-stream velocity was measured using a high-speed camera. These measurements were complemented by the measurements of unsteady velocity field with a high frame-rate Particle Image Velocimetry (PIV) system as well as smoke visualization. Membrane airfoils with excess length exhibit higher vibration modes, earlier roll-up of vortices, and smaller separated flow regions. whereas the membranes with pre-strain generally behave more similarly to a rigid airfoil. Measured frequencies of the membrane vibrations suggest a possible coupling with the wake instabilities at high incidences for all airfoils. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:359 / 376
页数:18
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