Structural Sizing Optimization of Aircraft Wing Structure Coupled with Direct Aeroelastic Mission Performance Sensitivity Analysis
- Weitere Titel
-
Strukturdickenoptimierung von Flugzeugflügelstrukturen gekoppelt mit einer direkten aeroelastischen Missionsleistungssensitivitätsanalyse
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- Umfang
-
Online-Ressource
- Sprache
-
Englisch
- Anmerkungen
-
München, Technische Universität München, Dissertation, 2023
- Schlagwort
-
Gestaltoptimierung
Flugzeugaerodynamik
Aeroelastizität
Strukturoptimierung
Aerodynamik
Finite-Elemente-Methode
- Ereignis
-
Veröffentlichung
- (wo)
-
München
- (wer)
-
Universitätsbibliothek der TU München
- (wann)
-
2023
- Urheber
-
Rechtik, Stephan
- Beteiligte Personen und Organisationen
- URN
-
urn:nbn:de:bvb:91-diss-20231218-1711647-1-8
- Rechteinformation
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
25.03.2025, 13:46 MEZ
Datenpartner
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Beteiligte
- Rechtik, Stephan
- Daoud, Fernaß
- Bletzinger, Kai-Uwe
- Universitätsbibliothek der TU München
Entstanden
- 2023
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