Efficient aeroelastic wing optimization through a compact aerofoil decomposition approach

to related objects

Location: Deutsche Nationalbibliothek Frankfurt am Main

ISSN: 1615-1488

Extent: Online-Ressource

Language: Englisch

Notes: online resource.

Bibliographic citation: 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

Creator: Poole, Daniel J.
Allen, Christian B.
Rendall, Thomas C. S.

Contributor: SpringerLink (Online service)

DOI: 10.1007/s00158-022-03174-4

URN: urn:nbn:de:101:1-2022060601354006585225

Rights: Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.

Last update: 15.08.2025, 7:32 AM CEST

Data provider

This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.

Show original at data provider

Associated

Poole, Daniel J.
Allen, Christian B.
Rendall, Thomas C. S.
SpringerLink (Online service)

Other Objects (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

Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads

HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS

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

Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads

HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS

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

Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads

HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS

Cultural heritage institutions wishing to register will find more information here.

Fields marked * need to be filled in.

Username*

Please enter your username

Email*

Please enter your email address

Please do not fill this field

First name

Last name

Password*

Please enter your password

Confirm password*

Please enter the same password

I have read the terms of use and the privacy policy for the collection of personal data and accept them. *

This field is required.

I would like to subscribe to the newsletter of the Deutsche Digitale Bibliothek. See newsletter subscription info.

Account created

Your "My DDB" account has been successfully created. Before you can log in to your account, you must click the confirmation link in the message we just sent to the email address you provided.

Efficient aeroelastic wing optimization through a compact aerofoil decomposition approach

Object Details

References and Relationships

Contributors, Places and Time

Further information

Data provider

Associated

Other Objects (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

Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads

HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS

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

Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads

HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS

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

Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads

HALO flight test with instrumented under-wing stores for aeroelastic and load measurements in the DLR project iLOADS

Related objects

Reset password