Neural network prediction and control of three-dimensional unsteady separated flowfields
One approach to the control of unsteady aerodynamics is to develop real-time models using artificial neural networks that anticipate the unsteady flowfield wing interactions. Evidence supporting this approach is presented.
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Veröffentlicht in: | Journal of aircraft 1995-11, Vol.32 (6), p.1213-1220 |
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container_title | Journal of aircraft |
container_volume | 32 |
creator | Faller, William E Schreck, Scott J Luttges, Marvin W |
description | One approach to the control of unsteady aerodynamics is to develop real-time models using artificial neural networks that anticipate the unsteady flowfield wing interactions. Evidence supporting this approach is presented. |
doi_str_mv | 10.2514/3.46866 |
format | Article |
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identifier | ISSN: 0021-8669 |
ispartof | Journal of aircraft, 1995-11, Vol.32 (6), p.1213-1220 |
issn | 0021-8669 1533-3868 |
language | eng |
recordid | cdi_pascalfrancis_primary_3007907 |
source | Alma/SFX Local Collection |
subjects | Aerodynamics Aircraft Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Neural networks Physics |
title | Neural network prediction and control of three-dimensional unsteady separated flowfields |
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