Rapid calculation of unsteady aircraft loads
Rapid calculation of unsteady aircraft loads
An efficient multi–fidelity aerodynamic solver for unsteady flow problems,
combining the unsteady vortex lattice method and Navier–Stokes solver for the infinite–swept wing problem, is presented. The new flow solver is able to correctly reproduce the loads of the three–dimensional Navier–Stokes unsteady, non–linear loads around a representative wing configuration, at a computational cost of a two–dimensional Navier–Stokes computation. Numerical details of the unsteady vortex lattice method solver, developed for this purpose, and its verification are presented. The coupling algorithm of multi–fidelity solver is described, followed by its demonstration around swept–wing configurations. It is demonstrated that the newly developed framework reproduces the loads of a three–dimensional unsteady Navier–Stokes computation, with the speed–up up
to 290–times for the same accuracy.
European Conference on Computational Mechanics
Drofelnik, Jernej
e785f695-61ef-4afc-bf0a-9dc7966f5516
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Kharlamov, Daniel
79b001cf-ae0a-4867-b38b-fcd73bb76bac
Sun, Yan
f99f12ab-7d43-4590-bfec-95e9d2855140
2018
Drofelnik, Jernej
e785f695-61ef-4afc-bf0a-9dc7966f5516
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Kharlamov, Daniel
79b001cf-ae0a-4867-b38b-fcd73bb76bac
Sun, Yan
f99f12ab-7d43-4590-bfec-95e9d2855140
Drofelnik, Jernej, Da Ronch, Andrea, Kharlamov, Daniel and Sun, Yan
(2018)
Rapid calculation of unsteady aircraft loads.
In 6th European Conference on Computational Mechanics (ECCM 6).
European Conference on Computational Mechanics.
12 pp
.
Record type:
Conference or Workshop Item
(Paper)
Abstract
An efficient multi–fidelity aerodynamic solver for unsteady flow problems,
combining the unsteady vortex lattice method and Navier–Stokes solver for the infinite–swept wing problem, is presented. The new flow solver is able to correctly reproduce the loads of the three–dimensional Navier–Stokes unsteady, non–linear loads around a representative wing configuration, at a computational cost of a two–dimensional Navier–Stokes computation. Numerical details of the unsteady vortex lattice method solver, developed for this purpose, and its verification are presented. The coupling algorithm of multi–fidelity solver is described, followed by its demonstration around swept–wing configurations. It is demonstrated that the newly developed framework reproduces the loads of a three–dimensional unsteady Navier–Stokes computation, with the speed–up up
to 290–times for the same accuracy.
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More information
Published date: 2018
Venue - Dates:
6th European Conference on Computational Mechanics (ECCM 6) & 7th European Conference on Computational Fluid Dynamics (ECFD 7), , Glasgow, United Kingdom, 2018-06-11 - 2018-06-15
Identifiers
Local EPrints ID: 484058
URI: http://eprints.soton.ac.uk/id/eprint/484058
PURE UUID: cad4656b-8023-4d76-9d23-a399e829c1e1
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Date deposited: 09 Nov 2023 17:58
Last modified: 18 Mar 2024 03:25
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Contributors
Author:
Jernej Drofelnik
Author:
Daniel Kharlamov
Author:
Yan Sun
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