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Surrogate Unsteady Aerodynamic Modeling with Autoencoders and Long-Short Term Memory Networks

  • Istanbul Technical University

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

13 Atıf (Scopus)

Özet

This paper presents preliminary results of an ongoing research in prediction of time-dependent flow fields by focusing on data-driven surrogate modeling using artificial neural networks for unsteady aerodynamic problems. The aim of this research is to model unsteady flow fields with learning in low-dimensional space and reconstruct with recurrent autoencoders. Within the scope of this paper, we separately share our findings in viscous unsteady flow field reconstruction of a 2D cylinder in a channel with a deep autoencoder and unsteady aerodynamic-acoustic time-series prediction of the supersonic NASA C25D aircraft with shallow long short-term memory networks. Satisfactory results are achieved in both unsteady applications, yet further improvements and validations are needed to be achieved to establish the desired surrogate unsteady aerodynamic modeling for supersonic aircraft maneuvers.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıAIAA SciTech Forum 2022
YayınlayanAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Basılı)9781624106316
DOI'lar
Yayın durumuYayınlandı - 2022
EtkinlikAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States
Süre: 3 Oca 20227 Oca 2022

Yayın serisi

AdıAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

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???event.eventtypes.event.conference???AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Ülke/BölgeUnited States
ŞehirSan Diego
Periyot3/01/227/01/22

Bibliyografik not

Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

Finansman

All authors would like to express their gratitude to TUBITAK for the research grant provided under the 218M471 TUBITAK 1001 project titled as "Development of Multifidelity and Multidisciplinary Methodologies Integrating Sonic Boom, Aeroelasticity and Propulsion System for Supersonic Aircraft Design".

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