A Computational Study of a Canonical Pitch-Up, Pitch-Down Wing Maneuver
By Jeff D. Eldredge, Chengjie Wang, M. Ol. 2009
198 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/4dfb24fd6a9843ec5a3abf3010de429084c26f20
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Low-order phenomenological modeling of leading-edge vortex formation (2013, unknown): “carried out both experimentally and computationally [12,16,19,35].”
- Discrete-vortex method with novel shedding criterion for unsteady aerofoil flows with intermittent leading-edge vortex shedding (2014, methodology): “The pitch–hold–return motion with sharp corners used here is generated using the Eldredge function (Eldredge et al. 2009) with a smoothing parameter a= 11.”