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

Numerical Simulation of Energy Flow between Insert Elements and Sandwich Panels with Honeycomb Core

Brysch, Marco und Wolff, Johannes (2014) Numerical Simulation of Energy Flow between Insert Elements and Sandwich Panels with Honeycomb Core. DLR-Interner Bericht. DLR-IB-FA-BS-2017-38. Masterarbeit. 84 S.

Dieses Archiv kann nicht den Volltext zur Verfügung stellen.

Kurzfassung

Sandwich panel structures are widely applied in engineering constructions due to their excellent Ratio between bending stiffness and bending strength. A high specialized structure requires large effort in manufacturing, what in turn leads to high costs. For this reason such structures are restricted to special applications, e.g. space vehicles and racing cars. Sandwich panels consists of a lightweight core which is covered by an upper and lower cover sheets. For the insert installation a hole is required in the sandwich panel. It showed that a slight disturbance of the bore hole center point affects the potting radius which is dependent on the insert hole diameter. As shown the ratio between the insert diameter and the cell size of the core determines the sensitivity of the potting geometry. A method is presented to reduce the uncertainties which arises in the insert installation process. A literature review on the insert elements, their application and Performance is presented. Then, the configuration of the sandwich structures such as assembling, core material and manufacturing are described. A base experimental characterization of the pull-out force of the sandwich panel is presented, where the experimental results are evaluated. A Simulation model using the Finite Element Method is setup. The modeling is extensively described, e.g. modeling of the cover sheet, insert element, potting, core and material definitions as well as the washer and screw force introductions. Finally, the numerical results are presented and compared with the experimental measurements. The occurrence of buckling processes in the simulation fits with analysis data from the experiment. In this way a determination of the linear elastic range and the start of plastic deformation in the core is possible.

elib-URL des Eintrags:https://elib.dlr.de/112433/
Dokumentart:Berichtsreihe (DLR-Interner Bericht, Masterarbeit)
Titel:Numerical Simulation of Energy Flow between Insert Elements and Sandwich Panels with Honeycomb Core
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Brysch, MarcoTU BraunschweigNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Wolff, JohannesJohannes.Wolff (at) dlr.dehttps://orcid.org/0000-0001-8775-9025NICHT SPEZIFIZIERT
Datum:Januar 2014
Referierte Publikation:Nein
Open Access:Nein
Seitenanzahl:84
Status:veröffentlicht
Stichwörter:Lasteinleitung, Sandwichbauweise, Simulation, Wabenkern, lokale Phänomene
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Verkehr
HGF - Programmthema:Bodengebundener Verkehr (alt)
DLR - Schwerpunkt:Verkehr
DLR - Forschungsgebiet:V BF - Bodengebundene Fahrzeuge
DLR - Teilgebiet (Projekt, Vorhaben):V - Next Generation Train III (alt), R - Raumfahrzeugsysteme - Konzepte und Entwurf (alt), L - Systeme und Kabine (alt), L - Strukturen und Werkstoffe (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Faserverbundleichtbau und Adaptronik > Funktionsleichtbau
Hinterlegt von: Böhringer-Thelen, Isolde
Hinterlegt am:18 Aug 2017 07:29
Letzte Änderung:18 Aug 2017 07:29

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

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