A procedure for obtaining steady-state solutions with WENO through sensitivity tuning and dynamic control

Blaine Vollmer, Daniel J. Bodony

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

Abstract

WENO schemes are known to struggle to obtain steady-state solutions in the presence of shocks. In this work, the 2D compressible Euler equations are solved using 5th-order finite difference WENO to obtain steady-state solutions by modifying the WENO parameters and implementing a dynamic weight controller. A descaling procedure is introduced to consistently compare and apply WENO across formulations and implementations. The response of WENO schemes to step inputs is studied to understand the effect of WENO parameters on weight activation and flux reconstruction. The effects on steady-state convergence and non-oscillatory behavior are then studied when the WENO parameters are varied. A PID control algorithm is introduced on the WENO weights that is capable of extending the ability of WENO to obtains teady solutions without introducing spatial oscillations.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum and Exposition, 2024
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624107115
DOIs
StatePublished - 2024
EventAIAA SciTech Forum and Exposition, 2024 - Orlando, United States
Duration: Jan 8 2024Jan 12 2024

Publication series

NameAIAA SciTech Forum and Exposition, 2024

Conference

ConferenceAIAA SciTech Forum and Exposition, 2024
Country/TerritoryUnited States
CityOrlando
Period1/8/241/12/24

ASJC Scopus subject areas

  • Aerospace Engineering

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