Unsteady aerodynamics and flow control for flapping wing flyers

By S. Hoa, Hany Nassefa, Nick Pornsinsirirakb, Yu-Chong Taib, Chih-Ming Hoa. 2003

469 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/1e5c73181f1676090ef10ecc0b0dc21d7d1a61f6

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. Bret K. Stanford
2. J. Hubner
3. Peter G. Ifju
4. R. Albertani

In Computational Mechanics

1. Bret K. Stanford

Citations in the corpus

• Aerodynamic Coefficients and Deformation Measurements on Flexible Micro Air Vehicle Wings (2007, background): “High spatial resolution data, as well as material properties, are necessary to accurately model the fluid-structure interactions of a deformable flying structure, either in vehicles or biological systems [21–23].”
• Analytical Sensitivity Analysis of an Unsteady Vortex Lattice Method for Flapping Wing Optimization (2009, unknown): “[9], Tuncer et al.”
• Bifurcating flows of plunging aerofoils at high Strouhal numbers (2012, unknown): “Aspects of the unsteady aerodynamics of oscillating aerofoils and wings and vortex-dominated flows have been reviewed by Shyy, Berg & Ljungqvist (1999), Triantafyllou, Triantafyllou & Yue (2000), Ho et al. (2003) and Platzer et al. (2008).”