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Reduced order models for aerodynamic applications, loads and MDO

Görtz, Stefan und Ripepi, Matteo und Franz, Thomas und Abu-Zurayk, Mohammad (2017) Reduced order models for aerodynamic applications, loads and MDO. 3rd Workshop on Model Reduction of Complex Dynamical Systems (MODRED 2017), 2017-01-11 - 2017-01-13, Odense, Dänemark.

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Kurzfassung

Reduced Order Models (ROMs) have found widespread application in fluid dynamics and aerodynamics. In their direct application to Computational Fluid Dynamics (CFD) ROMs seek to reduce the computational complexity of a problem by reducing the number of degrees of freedom rather than simplifying the physical model. Here, parametric nonlinear ROMs based on high-fidelity CFD are used to provide approximate flow solutions, but at lower evaluation time and storage than the original CFD model. ROMs for both steady and unsteady aerodynamic applications are presented. We consider ROMs combining proper orthogonal decomposition (POD) and Isomap, which is a manifold learning method, with interpolation methods as well as physics-based ROMs, where an approximate solution is found in the POD-subspace by minimizing the corresponding steady or unsteady flow-solver residual. In terms of the nonlinear unsteady least-squares ROM algorithm, we present the details of an improved accelerated greedy missing point estimation procedure which is usedin the online phase to select a subset of the unsteady residual for reasons of computational efficiency during the online prediction phase. The issue of how to best train the ROM with high-fidelity CFD data is also addressed. The goal is to train ROMs that yield a large domain of validity across all parameters and flow conditions at the expense of a relatively small number of CFD solutions. The different ROM methods are demonstrated on a wide-body transport aircraft configuration at transonic flow conditions. The steady ROMs are used to predict the static aeroelastic loads in the context of multidisciplinary optimization (MDO), where a structural model is to be sized for the (aerodynamic) loads. They are also used in a process where an a priori identification of the most critical static load cases is of interest and the sheer number of load cases to be considered does not lend itself to high-fidelity CFD. The unsteady nonlinear least-squares ROM approach is applied to modeling discrete gusts of different amplitude and length in the context of rapid evaluation of gust-induced air loads.

elib-URL des Eintrags:https://elib.dlr.de/110347/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Reduced order models for aerodynamic applications, loads and MDO
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Görtz, Stefanstefan.goertz (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Ripepi, Matteomatteo.ripepi (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Franz, Thomasthomas.franz (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Abu-Zurayk, Mohammadmohammad.abu-zurayk (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:11 Januar 2017
Referierte Publikation:Nein
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:CFD, MDO, loads, aerodynamics, steady, unsteady, reduced order models, ROMs, POD, isomap
Veranstaltungstitel:3rd Workshop on Model Reduction of Complex Dynamical Systems (MODRED 2017)
Veranstaltungsort:Odense, Dänemark
Veranstaltungsart:Workshop
Veranstaltungsbeginn:11 Januar 2017
Veranstaltungsende:13 Januar 2017
Veranstalter :University of Southern Denmark, Department of Mathematics and Computer Science (IMADA)
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Flugzeuge
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Aircraft Research
DLR - Teilgebiet (Projekt, Vorhaben):L - Simulation und Validierung (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > C²A²S²E - Center for Computer Applications in AeroSpace Science and Engineering
Hinterlegt von: Görtz, Stefan
Hinterlegt am:17 Jan 2017 13:56
Letzte Änderung:24 Apr 2024 20:15

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