Abstract
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.
Original language | English |
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Title of host publication | AIAA SciTech Forum 2022 |
Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
ISBN (Print) | 9781624106316 |
DOIs | |
Publication status | Published - 2022 |
Event | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States Duration: 3 Jan 2022 → 7 Jan 2022 |
Publication series
Name | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
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Conference
Conference | AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 |
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Country/Territory | United States |
City | San Diego |
Period | 3/01/22 → 7/01/22 |
Bibliographical note
Publisher Copyright:© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
Funding
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".