Neural-Network Surrogate Model for Flow Stability Analysis Based on Parabolized Stability Equations

Trenton S. Henderson, Devina P. Sanjaya, Gustavo Luiz Olichevis Halila, James G. Coder

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Scopus citations

Abstract

Use of artificial neural networks (ANN) for effectively modeling the Tollmien-Schlichting (TS) instabilities in transitional flow simulations has been investigated. This ANN surrogate model will enable an automated and robust framework for predicting the laminar-to-turbulent transition of boundary layers based on parabolized stability equations (PSE) and the N-factor envelope. Our goal is to couple the PSE-based transition model with the Spalart-Allmaras (SA) turbulence model and others used in aerodynamic design and optimization. Our results show that the proposed surrogate model can accurately predict the streamwise growth rate of perturbations for Falkner-Skan-Cooke (FSC) boundary layers. The N-factor computed based on the outputs of the ANN surrogate model is also sufficiently accurate to form a reliable N-factor envelope. We verify and validate our surrogate model on airfoil boundary layers by comparing it with available computational and experimental data for the NACA 0012 and NLF(1)-0416.

Original languageEnglish (US)
Title of host publicationAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624107238
DOIs
StatePublished - 2025
EventAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 - Orlando, United States
Duration: Jan 6 2025Jan 10 2025

Publication series

NameAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025

Conference

ConferenceAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
Country/TerritoryUnited States
CityOrlando
Period1/6/251/10/25

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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