elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Barrierefreiheit | Kontakt | English
Schriftgröße: [-] Text [+]

Vibration-correlation technique for predicting the compressive buckling load of cylindrical shells under combined loading

Baciu, Theodor und Franzoni, Felipe und Degenhardt, Richard und Gliszczynski, Adrian und Bisagni, Chiara (2025) Vibration-correlation technique for predicting the compressive buckling load of cylindrical shells under combined loading. Thin-Walled Structures, 216. Elsevier. doi: 10.1016/j.tws.2025.113576. ISSN 0263-8231.

Dieses Archiv kann nicht den Volltext zur Verfügung stellen.

Kurzfassung

The feasibility of the Vibration Correlation Technique (VCT) to predict the compressive buckling load of cylindrical shells under combined loading was numerically assessed. For this purpose, bending, shear, and torsion were applied in various amplitudes either individually, or simultaneously, next to the main compressive load for 6 cylinders. Then, the robustness of VCT to predict 1the axial load level at which buckling occurred under combined loading was assessed based on the prediction accuracy with respect to the buckling axial load level obtained through non-linear analysis, as well as on the differences in accuracy with respect to the predictions for the pure compression load case. The numerical investigation revealed that the VCT predictions of the buckling axial load level were robust for small degrees of additional load applied next to compression, regardless of the load type, loading sequence, or whether the additional load was taken into account or not when determining the reference critical buckling load needed to perform VCT. Furthermore, the VCT predictions were more robust when the vibration response reflected a change in the axial load level alone (sequential load introduction), particularly for bending. When additional bending was applied next to compression, taking into account this load in determining the critical buckling load improved the axial buckling load estimation, while for shear the opposite was observed. On the other hand, for torsion-compression this aspect remained unclear as it appeared cylinder specific.

elib-URL des Eintrags:https://elib.dlr.de/216501/
Dokumentart:Zeitschriftenbeitrag
Titel:Vibration-correlation technique for predicting the compressive buckling load of cylindrical shells under combined loading
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Baciu, Theodort.baciu (at) pfh.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Franzoni, FelipeFelipe.Franzoni (at) dlr.dehttps://orcid.org/0000-0002-9977-7607194688894
Degenhardt, RichardRichard.Degenhardt (at) dlr.dehttps://orcid.org/0000-0002-9766-9418NICHT SPEZIFIZIERT
Gliszczynski, Adrianadrian.gliszczynski1 (at) gmail.comNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Bisagni, ChiaraDipartimento di Ingegneria Aerospaziale, Politecnico di MilanoNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2025
Erschienen in:Thin-Walled Structures
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
Band:216
DOI:10.1016/j.tws.2025.113576
Verlag:Elsevier
ISSN:0263-8231
Status:veröffentlicht
Stichwörter:vibration correlation technique, shell buckling, combined loading
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - Projekt TRANSIENT, L - Strukturwerkstoffe und Bauweisen
Standort: Braunschweig
Institute & Einrichtungen:Institut für Systemleichtbau > Strukturmechanik
Hinterlegt von: Degenhardt, Prof. Dr. Richard
Hinterlegt am:20 Okt 2025 17:49
Letzte Änderung:20 Okt 2025 17:49

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
OpenAIRE Validator logo electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.