Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
5473065 | Aerospace Science and Technology | 2016 | 9 Pages |
Abstract
The onset and progression of vortex separation from a round leading edge on a moderately-swept diamond wing was investigated using the Zonal Detached Eddy Simulation (ZDES). Calculations were performed using mode 2 of ZDES that is appropriate for pressure-gradient-induced separation and that includes automated switching between the RANS and LES regions of the flow. The computations were performed early in conceptual design of the AVT-183 project to contribute unsteady flow assessments to other RANS-based steady flow simulations. The salient features of the roll-up of two vortex sheets are investigated together with a spectral analysis of the flow dynamics.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Sébastien Deck, James M. Luckring,