Hochschulschrift
Simulation-driven design of bonded joints in fibre composite aircraft structures using progressive damage analyses
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1434-8454
- Umfang
-
Online-Ressource
- Sprache
-
Englisch
- Anmerkungen
-
Braunschweig, Technische Universität Carolo-Wilhelmina, Dissertation, 2022
- Erschienen in
-
Forschungsbericht ; 2022-24
- Schlagwort
-
Finite-Elemente-Methode
Mechanisches Versagen
Klebeverbindung
Faserverbundwerkstoff
Leichtbau
Festigkeit
Laminat
- Ereignis
-
Veröffentlichung
- (wo)
-
Köln
- (wer)
-
Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Wissenschaftliche Information
- (wann)
-
2022
- Urheber
- Beteiligte Personen und Organisationen
-
Deutsches Zentrum für Luft- und Raumfahrt - Institut für Faserverbundleichtbau und Adaptronik
- DOI
-
10.57676/hya4-2a09
- URN
-
urn:nbn:de:101:1-2022112813203856745949
- Rechteinformation
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
25.03.2025, 13:48 MEZ
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Objekttyp
- Hochschulschrift
Beteiligte
- Völkerink, Oliver
- Deutsches Zentrum für Luft- und Raumfahrt - Institut für Faserverbundleichtbau und Adaptronik
- Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Wissenschaftliche Information
Entstanden
- 2022
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