Effect of flexure on aerodynamic propulsive efficiency of flapping flexible airfoil

By J. Miao, M. Ho. 2006

180 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/c05ab493a4f374fc76937afdf402eb3a36e6ffd8

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Hikaru Aono
2. Chang-kwon Kang
3. Wei Shyy
4. Carlos E. S. Cesnik
5. Pat Trizila
6. Hao Liu
7. S. Michelin
8. S. G. Smith

In Computational Mechanics

1. Wei Shyy
2. Hikaru Aono
3. Chang-kwon Kang
4. Carlos E. S. Cesnik
5. Pat Trizila
6. S. Michelin
7. Hao Liu
8. S. G. Smith

Citations in the corpus

• Resonance and propulsion performance of a heaving flexible wing (2009, background): “In such experimental [12, 13], theoretical [1, 14] and numerical studies [15, 16, 17, 18], the position of the solid is prescribed and the influence of the swimming stroke on the propulsive performance is analyzed.”
• Recent progress in flapping wing aerodynamics and aeroelasticity (2010, background): “Miao and Ho [237] prescribed a time-dependent flexible deformation profile for an airfoil in pure plunge and investigated the effect of flexure amplitude on the unsteady aerodynamic characteristics for various combinations of Reynolds number and reduced frequency.”
• Optimal flexibility of a flapping appendage in an inviscid fluid (2008, methodology): “Miao & Ho (2006) used a dynamic conformal mesh to study a flexible airfoil in a heaving motion at Reynolds numbers of O(104).”