High fidelity computational simulation of a membrane wing airfoil

By R. Gordnier. 2008

174 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/8b31564806a8a3bb269cd50b419a5bce2a05b32b

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. Zhijin Wang
2. Pinunta Rojratsirikul
3. I. Gursul
4. Rye M. Waldman
5. A. Carrere
6. O. Curet
7. K. Breuer
8. Wei Shyy

In Computational Mechanics

1. Zhijin Wang
2. Pinunta Rojratsirikul
3. Rye M. Waldman
4. A. Carrere
5. K. Breuer
6. O. Curet
7. I. Gursul
8. Wei Shyy

Citations in the corpus

• Flow-induced vibrations of low aspect ratio rectangular membrane wings (2011, background): “The close coupling between vortex shedding and membrane response was also demonstrated in simulations by Gordnier (2009).”
• Unsteady fluid–structure interactions of membrane airfoils at low Reynolds numbers (2009, methodology): “Although the effect of Re and P could not be separated in these experiments, this was done in the numerical simulations by Gordnier (2008) .”
• Aerodynamic Characterization of a Wing Membrane with Variable Compliance (2014, methodology): “There has been recent progress in the study of membrane wings [10,12–16].”
• Aeromechanics of Membrane Wings with Implications for Animal Flight ArnoldSong, ∗ XiaodongTian, † EmilyIsraeli, ‡ RicardoGalvao, § KristinBishop, ¶ SharonSwartz, ∗∗ (2008, background): “This difference is probably due to the compliance of the wing, which appears to change the character of the separated vortex structure [29].”