Surrogate models for predicting noise emission and aerodynamic performance of propellers
Created by W.Langdon from
gp-bibliography.bib Revision:1.8051
- @Article{POGGI:2021:AST,
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author = "Caterina Poggi and Monica Rossetti and
Giovanni Bernardini and Umberto Iemma and Cristiano Andolfi and
Christian Milano and Massimo Gennaretti",
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title = "Surrogate models for predicting noise emission and
aerodynamic performance of propellers",
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journal = "Aerospace Science and Technology",
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year = "2021",
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volume = "125",
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pages = "107016",
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month = jun,
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keywords = "genetic algorithms, genetic programming, Propeller
aerodynamics and aeroacoustics, Surrogate models,
Artificial Neural Network, ANN",
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ISSN = "1270-9638",
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URL = "https://ui.adsabs.harvard.edu/abs/2022AeST..12507016P/abstract",
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URL = "https://www.sciencedirect.com/science/article/pii/S1270963821005265",
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DOI = "doi:10.1016/j.ast.2021.107016",
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abstract = "This paper deals with the innovative development of
surrogate models suitable for the simulation of
aerodynamic performance and acoustic emission in terms
of tonal components, of multi-propeller systems like
those applicable in urban air-mobility vehicles. These
can be of great help particularly when designing
distributed-electric-propulsion configurations, as they
provide an agile tool that avoids the need for
computationally expensive CFD/CAA predictions. Without
losing the generality of the conclusions that can be
drawn about the capability of the proposed surrogate
models to accurately describe multi-propeller
aerodynamic and aeroacoustic responses, applications to
a single propeller configuration are presented.
Focusing on the simulation of the effects due to the
spanwise distribution of blade twist and chord length,
two surrogate modelling techniques are examined: one
based on Artificial Neural Networks and one based on
Genetic Programming. The numerical database for the
identification of these models is determined by the
combined application of a boundary integral formulation
suitable for the potential aerodynamics solution around
lifting/thrusting bodies, and the Farassat 1A
formulation for the evaluation of the noise field. The
numerical investigation demonstrates that both
metamodelling techniques are able to reproduce
propeller aerodynamic performance and radiated noise
with a very good level of accuracy, certainly suitable
for preliminary design applications",
- }
Genetic Programming entries for
Caterina Poggi
Monica Rossetti
Giovanni Bernardini
Umberto Iemma
Cristiano Andolfi
Christian Milano
Massimo Gennaretti
Citations