Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: Implementation and validation
By Salman Ahmad Ansari, R. Żbikowski, Kevin Knowles. 2006
137 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/8b864c65a2deb0e6bf68c29dece12813abd3a8dc
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding (2014, methodology): “In the current method, the placement methodology given by Ansari et al. (2006a) and Ansari, Żbikowski & Knowles (2006b) is used, where the latest vortex is placed at one-third of the distance from the shedding edge to the previously shed vortex.”