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Data-driven prediction of forced-motion unsteady aerodynamic surface quantities using graph neural ordinary differential equations

Lange, Henrik und Bekemeyer, Philipp (2026) Data-driven prediction of forced-motion unsteady aerodynamic surface quantities using graph neural ordinary differential equations. WCCM ECCOMAS 2026, 2026-07-19 - 2026-07-24, München, Deutschland. (nicht veröffentlicht)

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Kurzfassung

Unsteady aerodynamic phenomena such as gusts and flutter impose significant loads on aircraft and must be predicted accurately during design, certification, and optimisation. Although higher-fidelity methods like solving the unsteady Reynolds-Averaged Navier-Stokes (URANS) equations or large-eddy simulations can capture complex unsteady behaviour, including dynamic non-linearities, their computational cost is prohibitive for many-query applications. Machine learning (ML)-based surrogate models offer a promising alternative, combining the ability to capture non-linear relationships with fast evaluation once trained. For computational fluid dynamics the spatial domain is discretised as a mesh. Graph neural networks (GNNs) are a ML method that can exploit the mesh structure as an inductive bias [1, 2]. This work introduces an URANS-based dataset containing multiple trajectories of unsteady pitch and heave motions of a two-dimensional airfoil with varying amplitudes, frequencies, and initial conditions. The goal is to find a surrogate model that predicts surface quantities (pressure and skin friction) given a steady initial flow solution and an exogenous input signal that describes the airfoil’s motion in time. Initial investigations that extend the approach from [2] with exogenous inputs identified the error accumulation of the autoregressive model as the main limitation for long roll-outs in time. Several approaches to mitigate this problem are investigated. Firstly, architectural adaptations such as the integration of temporal ML components (Gated Recurrent Units or temporal attention) inside the GNN structure are explored. Secondly, training methodologies are evaluated. Finally, the approach is reformulated as a neural ordinary differential equation (Neural ODE) [3], combining strengths of classical numerical methods with ML. While the first two approaches lead to some improvements, preliminary results on the latter approach look most promising.

elib-URL des Eintrags:https://elib.dlr.de/227820/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Data-driven prediction of forced-motion unsteady aerodynamic surface quantities using graph neural ordinary differential equations
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Lange, Henrikh.lange (at) dlr.dehttps://orcid.org/0009-0002-9295-7346NICHT SPEZIFIZIERT
Bekemeyer, PhilippPhilipp.Bekemeyer (at) dlr.dehttps://orcid.org/0009-0001-9888-2499NICHT SPEZIFIZIERT
Datum:20 Juli 2026
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:nicht veröffentlicht
Stichwörter:surrogate model, unsteady aerodynamics, graph neural network, neural ordinary differential equation, deep learning, spatio-temporal modelling
Veranstaltungstitel:WCCM ECCOMAS 2026
Veranstaltungsort:München, Deutschland
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:19 Juli 2026
Veranstaltungsende:24 Juli 2026
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Effizientes Luftfahrzeug
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L EV - Effizientes Luftfahrzeug
DLR - Teilgebiet (Projekt, Vorhaben):L - Virtuelles Flugzeug und Validierung
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > CASE, BS
Hinterlegt von: Lange, Henrik
Hinterlegt am:14 Okt 2026 09:20
Letzte Änderung:14 Okt 2026 09:20

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