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
Hauptverfasser: Faller, William E, Schreck, Scott J, Luttges, Marvin W
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container_issue 6
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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
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identifier ISSN: 0021-8669
ispartof Journal of aircraft, 1995-11, Vol.32 (6), p.1213-1220
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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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