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Aeroelastic Design and Optimization of Green Aircraft

Krüger, Wolf R. (2013) Aeroelastic Design and Optimization of Green Aircraft. International Forum of Aeroelasticity and Structural Dynamics (IFASD), 24.-27.6.2013, Bristol.

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Aeroelastic effects play a large role in aircraft development, where the necessity to minimize fuel consumption and emissions creates a pressure to move towards light weight structures and new technical solutions like laminar flow wings for transonic aircraft. DLR is performing a series of investigations on the impact of so-called “green” technologies on aeroelastic stability and dynamic loads. One aspect of those investigations is the improvement of corresponding numerical analysis approaches, from fast methods to high fidelity methods, and the experimental validation of those approaches. Furthermore, aeroelasticity is seen as a design driver - aeroelastic tailoring and active loads control are examples of the mutual interaction between aeroelasticity and aircraft design & optimization. The presentation will give an overview of current DLR activities in the field of aeroelastic analysis, design and optimization, with examples of applications from DLR-, German national-, and European projects.

Item URL in elib:https://elib.dlr.de/83272/
Document Type:Conference or Workshop Item (Speech)
Additional Information:invited keynote presentation
Title:Aeroelastic Design and Optimization of Green Aircraft
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Krüger, Wolf R.Wolf.Krueger (at) dlr.deUNSPECIFIED
Date:June 2013
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:aircraft design; aeroelasticity; green aircraft
Event Title:International Forum of Aeroelasticity and Structural Dynamics (IFASD)
Event Location:Bristol
Event Type:international Conference
Event Dates:24.-27.6.2013
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research (old)
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics (old)
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Deposited By: Krüger, Prof. Dr.-Ing. Wolf R.
Deposited On:05 Aug 2013 10:58
Last Modified:08 May 2014 23:24

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