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Krüger, Wolf R. and Klimmek, Thomas and Liepelt, René and Schmidt, Hauke and Waitz, Stefan and Cumnuantip, Sunpeth (2014) Design and aeroelastic assessment of a forward-swept wing aircraft. CEAS Aeronautical Journal, 5 (4), pp. 419-433. Springer. doi: 10.1007/s13272-014-0117-0. ISSN 1869-5582.
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Official URL: http://link.springer.com/article/10.1007%2Fs13272-014-0117-0
Abstract
Aeroelastic effects strongly influence the design of an aircraft. To be able to assess those effects early on, reliable simulation models representing the global aeroelastic properties of a new design are required. At a conceptual or a pre-design stage, an intelligent parameterization concept allows for limited changes of the configuration while the simulation models are adapted accordingly. In the DLR project Integrated Green Aircraft, the goal was to investigate the impact of technologies for the reduction of fuel consumption on the aeroelastic properties of aircraft. One main aspect was the influence of laminar wing design on divergence, flutter and dynamic loads. As the reference aircraft in the project, the concept of a forward-swept wing aircraft with rear-mounted engines has been analysed. An aeroelastic model has been built up in the project. The model design procedure is based on the DLR in-house tool set MONA (ModGen/ NASTRAN). Focus of this design process is the generation of a parameterized structural model, representing the global dynamic properties of the elastic aircraft, but as detailed as reasonable to capture relevant local effects and to result in a feasible structural design. In the article, the aircraft design is presented. The modelling and sizing process for the structure is described. Results of the loads analysis as well as of the aeroelastic stability analyses are discussed.
| Item URL in elib: | https://elib.dlr.de/89913/ | |||||||||||||||||||||
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| Document Type: | Article | |||||||||||||||||||||
| Additional Information: | Springer-Publikation "Online-first" | |||||||||||||||||||||
| Title: | Design and aeroelastic assessment of a forward-swept wing aircraft | |||||||||||||||||||||
| Authors: |
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| Date: | December 2014 | |||||||||||||||||||||
| Journal or Publication Title: | CEAS Aeronautical Journal | |||||||||||||||||||||
| Refereed publication: | Yes | |||||||||||||||||||||
| Open Access: | No | |||||||||||||||||||||
| Gold Open Access: | No | |||||||||||||||||||||
| In SCOPUS: | Yes | |||||||||||||||||||||
| In ISI Web of Science: | No | |||||||||||||||||||||
| Volume: | 5 | |||||||||||||||||||||
| DOI : | 10.1007/s13272-014-0117-0 | |||||||||||||||||||||
| Page Range: | pp. 419-433 | |||||||||||||||||||||
| Publisher: | Springer | |||||||||||||||||||||
| ISSN: | 1869-5582 | |||||||||||||||||||||
| Status: | Published | |||||||||||||||||||||
| Keywords: | forward-swept wings, aeroelastic design, rear-mounted engines, parametric modelling | |||||||||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | |||||||||||||||||||||
| HGF - Program: | Aeronautics | |||||||||||||||||||||
| HGF - Program Themes: | fixed-wing aircraft | |||||||||||||||||||||
| DLR - Research area: | Aeronautics | |||||||||||||||||||||
| DLR - Program: | L AR - Aircraft Research | |||||||||||||||||||||
| DLR - Research theme (Project): | L - Flexible Aircraft (old) | |||||||||||||||||||||
| Location: | Göttingen | |||||||||||||||||||||
| Institutes and Institutions: | Institute of Aeroelasticity | |||||||||||||||||||||
| Deposited By: | Krüger, Prof. Dr.-Ing. Wolf R. | |||||||||||||||||||||
| Deposited On: | 07 Aug 2014 13:28 | |||||||||||||||||||||
| Last Modified: | 06 Sep 2019 15:24 |
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