Time-resolved reconstruction of the full velocity field around a dynamically-scaled flapping wing
By Christian Poelma, William B. Dickson, Michael H. Dickinson. 2006
208 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/006739ecf1cdead2b13ab469021dfd2e509886dc
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
- Wei Shyy
- Chang-kwon Kang
- Carlos E. S. Cesnik
- Pat Trizila
- Hao Liu
- Satish Kumar Chimakurthi
- M. Ol
In Computational Mechanics
- Wei Shyy
- Hikaru Aono
- Kunihiko Taira
- Chang-kwon Kang
- Carlos E. S. Cesnik
- Tim Colonius
- R. Monchaux
- Pat Trizila
Citations in the corpus
- Recent progress in flapping wing aerodynamics and aeroelasticity (2010, background): “[72] measured the time-dependent 3-D velocity field around a flapping wing at Re=256 based on maximum chord.”
- Shallow and deep dynamic stall for flapping low Reynolds number airfoils (2009, background): “2008) is to quantitatively ascertain the role of two-dimensional effects such as leading edge vortex formation and vortex shedding, and three-dimensional effects such as spanwise relief in leading edge vortices (Usherwood and Ellington 2002) and leading–trailing edge vortex interaction was made poss”
- Analyzing preferential concentration and clustering of inertial particles in turbulence (2012, background): “For dilute conditions, significant progresses have been achieved in that direction which are mostly based on 2D imaging (see for example (Yang and Shy, 2005; Poelma et al., 2006; Zhou and Chang, 2009), with some contributions now emerging on imaging 3D fields (for example Guala et al.”
- Reynolds number and aspect ratio effects on the leading-edge vortex for rotating insect wing planforms (2013, methodology): “This spanwise velocity pattern is similar to those observed by Birch et al. (2004) and Poelma et al. (2006).”
- Three-dimensional flows around low-aspect-ratio flat-plate wings at low Reynolds numbers (2009, background): “Stable attachment of the leading-edge vortices on flapping wings has been observed to provide enhanced lift for prolonged duration (Birch et al. 2004; Poelma et al. 2006 ).”