A Multi-fidelity Prediction with Convolutional Neural Networks Using High-Dimensional Data

Huseyin Emre Tekaslan, Melike Nikbay

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Citations (Scopus)

Abstract

This paper proposes two novel multi-fidelity neural network architectures tailored for high-dimensional inputs such as computational flow fields. The proposed methods are compared with the multi-fidelity deep neural networks from the literature using a 2-dimensional flow-varying supercritical airfoil problem. The main objective of this study is to generate a multi-fidelity prediction of aerodynamic coefficients using pressure coefficient fields around the airfoil. To generate the dataset, a coarse grid is solved using SU2 Euler solver for low-fidelity data whereas a relatively finer grid is utilized for high-fidelity data to obtain viscous solutions using the Spallart-Allmaras turbulence model. The performance metrics to compare the methods are determined as the test accuracy, physical training time, and the size of the high-fidelity samples. Results demonstrate that the proposed multi-fidelity neural network architectures outperform the multi-fidelity deep neural networks in predictive modeling using high dimensional inputs by improving the multi-fidelity prediction accuracy up to 78.7%.

Original languageEnglish
Title of host publicationAIAA AVIATION 2022 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106354
DOIs
Publication statusPublished - 2022
EventAIAA AVIATION 2022 Forum - Chicago, United States
Duration: 27 Jun 20221 Jul 2022

Publication series

NameAIAA AVIATION 2022 Forum

Conference

ConferenceAIAA AVIATION 2022 Forum
Country/TerritoryUnited States
CityChicago
Period27/06/221/07/22

Bibliographical note

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

Funding

The authors would like to express their gratitude to General Electric Gas Power, UK, for the research grant titled "Development of Convolutional Neural Network Based Predictive Modeling Code". The authors would also like to acknowledge TUBITAK for the research grant provided under the 218M471 TUBITAK 1001 project titled "Development of Multi-fidelity and Multidisciplinary Methodologies Integrating Sonic Boom, Aeroelasticity and Propulsion System for Supersonic Aircraft Design".

Fingerprint

Dive into the research topics of 'A Multi-fidelity Prediction with Convolutional Neural Networks Using High-Dimensional Data'. Together they form a unique fingerprint.

Cite this