Membrane Wing-Based Micro Air Vehicles

By Wei Shyy, Peter G. Ifju, Dragos Viieru. 2005

163 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Condensed Matter Physics

View Paper: https://www.semanticscholar.org/paper/e431a0448a2376d1674bc161902770cf3d3f299f

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. K. Breuer
6. Pat Trizila
7. Hao Liu
8. Rye M. Waldman

In Condensed Matter Physics

1. K. Breuer
2. Carlos E. S. Cesnik
3. Wei Shyy
4. Chang-kwon Kang
5. Hikaru Aono

Citations in the corpus

• Aeromechanics of Membrane Wings with Implications for Animal Flight ArnoldSong, ∗ XiaodongTian, † EmilyIsraeli, ‡ RicardoGalvao, § KristinBishop, ¶ SharonSwartz, ∗∗ (2008, methodology): “As has been pointed out before [22], to”
• Aerodynamic Characterization of a Wing Membrane with Variable Compliance (2014, background): “In recent years, there has been substantial progress in the development ofmicro air vehicles (MAVs) [7].”
• Recent progress in flapping wing aerodynamics and aeroelasticity (2010, background): “On the aerodynamics side, in a fixed wing set-up, wind tunnel measurements show that corrugated wings are aerodynamically insensitive to the Reynolds number variations, which is quite different from a typical low Reynolds number airfoil [1,4,6,7,12].”