Efficient aeroelastic wing optimization through a compact aerofoil decomposition approach
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1615-1488
- Umfang
-
Online-Ressource
- Sprache
-
Englisch
- Anmerkungen
-
online resource.
- Erschienen in
-
Efficient aeroelastic wing optimization through a compact aerofoil decomposition approach ; volume:65 ; number:3 ; day:8 ; month:2 ; year:2022 ; pages:1-19 ; date:3.2022
Structural and multidisciplinary optimization ; 65, Heft 3 (8.2.2022), 1-19, 3.2022
- Urheber
-
Poole, Daniel J.
Allen, Christian B.
Rendall, Thomas C. S.
- Beteiligte Personen und Organisationen
-
SpringerLink (Online service)
- DOI
-
10.1007/s00158-022-03174-4
- URN
-
urn:nbn:de:101:1-2022060601354006585225
- Rechteinformation
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
14.06.2025, 01:56 MESZ
Datenpartner
Dieses Objekt wird bereitgestellt von:
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Beteiligte
- Poole, Daniel J.
- Allen, Christian B.
- Rendall, Thomas C. S.
- SpringerLink (Online service)
Ähnliche Objekte (12)
Aeroelastic method to investigate nonlinear elastic wing structures
Aeroelastic behaviour of a wing with over-the-wing mounted UHBR engine
Reliability-based aeroelastic design of composite plate wings using a stability margin
Nonlinear metamaterial enabled aeroelastic vibration reduction of a supersonic cantilever wing plate
An aeroelastic optimisation framework for manufacturable variable stiffness composite wings including critical gust loads
Aeroelastic simulations of a delta wing with a Chimera approach for deflected control surfaces
Static aeroelastic stiffness optimization of a forward swept composite wing with CFD-corrected aero loads
Structural Sizing Optimization of Aircraft Wing Structure Coupled with Direct Aeroelastic Mission Performance Sensitivity Analysis
Efficient and practical modular decomposition
Basement membrane mechanics in the Drosophila wing disc epithelium
HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS
Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads
Aeroelastic method to investigate nonlinear elastic wing structures
Aeroelastic behaviour of a wing with over-the-wing mounted UHBR engine
Reliability-based aeroelastic design of composite plate wings using a stability margin
Nonlinear metamaterial enabled aeroelastic vibration reduction of a supersonic cantilever wing plate
An aeroelastic optimisation framework for manufacturable variable stiffness composite wings including critical gust loads
Aeroelastic simulations of a delta wing with a Chimera approach for deflected control surfaces
Static aeroelastic stiffness optimization of a forward swept composite wing with CFD-corrected aero loads
Structural Sizing Optimization of Aircraft Wing Structure Coupled with Direct Aeroelastic Mission Performance Sensitivity Analysis
Efficient and practical modular decomposition
Basement membrane mechanics in the Drosophila wing disc epithelium
HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS
Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads
Aeroelastic method to investigate nonlinear elastic wing structures
Aeroelastic behaviour of a wing with over-the-wing mounted UHBR engine
Reliability-based aeroelastic design of composite plate wings using a stability margin
Nonlinear metamaterial enabled aeroelastic vibration reduction of a supersonic cantilever wing plate
An aeroelastic optimisation framework for manufacturable variable stiffness composite wings including critical gust loads
Aeroelastic simulations of a delta wing with a Chimera approach for deflected control surfaces
Static aeroelastic stiffness optimization of a forward swept composite wing with CFD-corrected aero loads
Structural Sizing Optimization of Aircraft Wing Structure Coupled with Direct Aeroelastic Mission Performance Sensitivity Analysis
Efficient and practical modular decomposition
Basement membrane mechanics in the Drosophila wing disc epithelium
HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS