Analytical Sensitivity Analysis of an Unsteady Vortex Lattice Method for Flapping Wing Optimization

By Bret K. Stanford, Philip S. Beran. 2009

158 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/6f508208313095430a658317151c9789aecafd7e

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. Julia Maria Graham
2. Rafael Palacios
3. J. Murua
4. Muhammad R. Hajj
5. Haithem E. Taha
6. Ali H. Nayfeh

In Computational Mechanics

1. Julia Maria Graham
2. Rafael Palacios
3. Muhammad R. Hajj
4. J. Murua
5. Haithem E. Taha
6. Ali H. Nayfeh
7. Abdessattar Abdelkefi
8. Lin Wang

Citations in the corpus

• Wing Kinematics Optimization for Hovering Micro Air Vehicles Using Calculus of Variation (2013, methodology): “Stanford and Beran [13] performed a gradient-based optimization of flapping-wing active shape morphing in forward flight.”
• Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics (2012, background): “Hence, while the DLM has dominated in fixed-wing aircraft aeroelasticity, the UVLM has been gaining ground in situations where free-wake methods become a necessity because of geometric complexity, such as flapping-wing kinematics [69–71], rotorcraft [72, 73], or wind turbines [74–80].”