Flapping Wings and Aerodynamic Lift: The Role of Leading-Edge Vortices
257 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/70f5444e1358e4bfb57ef9cd1c2bbb38a0f5c222
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
- Hikaru Aono
- Chang-kwon Kang
- Wei Shyy
- Carlos E. S. Cesnik
- Pat Trizila
- Hao Liu
- Satish Kumar Chimakurthi
- Rafael Palacios
In Computational Mechanics
- Wei Shyy
- Hikaru Aono
- Chang-kwon Kang
- Carlos E. S. Cesnik
- Pat Trizila
- Hao Liu
- Satish Kumar Chimakurthi
- Timothy Reis
Citations in the corpus
- Can Tip Vortices Enhance Lift of a Flapping Wing (2009, background): “Wake capture depends strongly on the wing kinematics [6], and performance of delayed stall is affected seriously by the stability of theLEV [4,7] aswell as theflowparameters such as the Reynolds number [3,8].”
- Unsteady force generation and vortex dynamics of pitching and plunging aerofoils (2012, unknown): “8 low Re are documented in numerical studies that support the observations made in experiments [49,50].”
- Recent progress in flapping wing aerodynamics and aeroelasticity (2010, methodology): “D NS computations, Liu and Aono [42] and Shyy and Liu [65] demonstrated that a LEV is a common flow feature in flapping wing aerodynamics at Reynolds numbers O(104) and lower, which correspond to the flight regime of insects and flapping wing MAVs.”