High-order simulations of low Reynolds number membrane airfoils under prescribed motion
- 作者：Justin W. Jaworski ; jwj@alumni.duke.edu ; Raymond E. Gordnier raymond.gordnier@wpafb.af.mil
- 关键词：Flapping propulsion ; Membrane wing ; Micro air vehicle ; Vortex dynamics ; Navier&ndash ; Stokes simulations
- 刊名：Journal of Fluids and Structures
- 出版年：2012
- 期刊代码：187_08899746
- 类别：et
- 出版时间：May, 2012
- 卷：31
- 期：Complete
- 页码：49-66
- 文件大小：1672 K
摘要
The aerodynamics and aeroelastic response of a membrane wing under prescribed motion are investigated using a high-order, two-dimensional Navier-Stokes solver coupled to a geometrically nonlinear membrane model. The impact of increasing Reynolds number on the vortex dynamics and unsteady aerodynamic loads is examined for moderate-amplitude plunge and combined pitch-plunge motions at low frequency. Simulation results are compared with classical thin airfoil theory and highlight the differences between rigid and flexible membrane airfoils undergoing small and moderate amplitude motions. The present study demonstrates the ability of lifting membrane surface flexibility to enhance thrust production and propulsive efficiency, which may inform the design of flapping wing membrane fliers.